N830WA

Part: BATTERY — DISCHARGED (CABIN) · airframe 73,731 hrs · 44,581 cycles

OVERWING EMERGENCY LIGHT SIGNS BLINKING. REPLACED BATTERY PACK

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,589 hrs · 44,495 cycles

FUSELAGE FRAME STA 760, AN UNIDENTIFIED REPAIR WAS REMOVED FROM THE FS 760 LT OVERWING EXIT FRAME. THE FRAME WAS FOUND WITH A TYPICAL CRACK PER BAC S/B 727-53-0197. A NEW FRAME REPAIR WAS INSTALLED PER THE REQUIREMENTS OF THE S/B AND PER ER/A 382044-14AD, REV A.

Part: BEAM — CRACKED (FUSELAGE) · airframe 73,589 hrs · 44,495 cycles

BULKHEAD FS 1183 VERTICAL BEAM RBL 8 WL 182 CRACKED. THE RBL 8 VERTICAL BEAM ON THE FS 1183 BULKHEAD WAS FOUND WITH A 1 INCH CRACK AT THE LOWER END AT WL 182. THE CRACK IS TYPICAL OF BAC SB 727-53-0175. THE CRACK WAS REPAIRED PER THE SB AND PER ER/A 382022-14.

Part: ATTACH ANGLE — CRACKED (L/E SLAT) · airframe 73,589 hrs · 44,495 cycles

1/4 INCH CRACK IN NR 1 SLAT COVE SKIN LWR ATTACH ANGLE BELOW TAI DUCT. REPAIRED PER 727 M/M 57-54-000-8 FIG 805A

Part: SIGN — INOPERATIVE (COCKPIT) · airframe 73,308 hrs · 44,311 cycles

EMERGENCY EXIT SIGN OVER WINDOW EXIT, CAPTS SIDE, AFT EXIT INOP. RELAMPED.

Part: SIGN — INOPERATIVE (L1 DOOR) · airframe 73,308 hrs · 44,311 cycles

EMERGENCY EXIT SIGN OVER L1 INOP. RELAMPED.

Part: FAN — FAILED (CARGO BAY) · airframe 72,799 hrs · 43,962 cycles

ELECTRICAL SMELL NOTED FROM ROWS 25, GASPER FAN C/B POPPED. REPLACED GASPER FAN.

Part: BATTERY PACK — INOPERATIVE (L2 DOOR) · airframe 72,009 hrs · 43,436 cycles

INTERIOR L2 DOOR EMER LITE INOPERATIVE - REPLACED POWER SUPPLY BATTERY PACK.

Part: ATTACH ANGLE — CRACKED (SLAT) · airframe 71,745 hrs · 43,268 cycles

A .5 INCH VISIBLE CRACK AT I/B STOP ATTACH ANGLE ON NR 7 L/E SLAT. REPAIRED PER MM 57-54-000-8.

Part: GYRO — INOPERATIVE (COCKPIT) · airframe 70,412 hrs · 42,439 cycles

CAPTS ATTITUDE GYRO FAILS IN TURNS THAT EXCEED 10 DEG OF BANK. REPLACED NR 1 VG AND CAPTS ADI TEST OK PER MM 34-22-21.

Part: CONTROLLER — INOPERATIVE (COCKPIT) · airframe 69,065 hrs · 41,558 cycles

UNABLE TO PRESSURIZE CABIN IN AUTO/STBY OR MANUAL MODE. RAN ENGS PER PFHB, AIRCRAFT PRESSURIZED NORMALLY AND NO LEAKS FOUND.

Part: WEB — CRACKED (TORQUE BOX)

TWO CRACKS AT LIGHTENING HOLES RT TORQUE BOX VERT WEB STA 1223 AT UPPER LIGHTENING HOLE AND STA 1233 AT LOWER LIGHTENING HOLE. REPAIRED PER MM 53-11-0.

Part: WEB — CRACKED (TORQUE BOX)

A .25 INCH CRACK AT LT TORQUE BOX VERT WEB LWR LIGHTENING HOLE STA 1233. TWO .1875 INCH CRACKS AT LT TORQUE BOX VERT WEB UPPER LIGHTENING HOLE STA 1223. BOTH REPAIRED PER MM 53-11-0.

Part: BATTERY — DISCHARGED (CABIN)

F/C CABIN OVERHEAD EMERGENCY LIGHT INOP. C/W REPLACED BATTERY PACK.

Part: BATTERY — DISCHARGED (R2 DOOR)

EMERGENCY LIGHT AT R2 DOOR INOP. C/W REPLACED BATTERY PACK.

Part: BATTERY — DISCHARGED (AFT AIRSTAIR)

AFT AIRSTAIR EMERGENCY LIGHT INOP. C/W REPLACED BATTERY PACK.

Part: VALVE — LEAKING (A HYD SYS)

ON SHORT FINAL LOST ALL A HYD QTY AND PRESSURE. REPLACED FLOW REGULATOR VALVE, NR 1 AND 2 CASE DRAIN FILTERS SERVICED A HYD AND RAN ENGS. ALL INDICATIONS AND OPERATION CHECKS OK LEAK CHECKS OK.

Part: SKIN — WORN (BS 950)

LOWER SKIN BELOW THE WING TO BODY FAIRING AT BS 950D BETWEEN S26R AND S27R WAS FOUND DAMAGED DUE TO A LOOSE FASTENER. REPAIRED PER ERA 333123-14, REV A.

Part: SKIN — CORRODED (BS 720)

FUSELAGE SKIN FOUND WITH CORROSION AT BS 720E AND S26R. ONLY THE LOWER (OVERLAPPED) SKIN WAS DAMAGED. REPAIRED PER ERA 333122-14, REV B.

Part: FRAME — MISDRILLED (BS 784)

WHILE PERFORMING REPETITIVE INSP PER OPN 5865 REQD BY AD 94-02-04 (REF 4-61904-3AD/-12AD) AN OVERSIZED FASTENER HOLE WAS FOUND IN THE RT BS 784 FRAME, I/B CHORD. THE SUBJECT HOLE IS THE 2ND BELOW THE FLOOR LINE. NO CRACKS WERE FOUND. REWORKED PER ERA 333135-14AD, REV A.

Part: SKIN — DAMAGED (BS 380)

DURING HMV, A T/L REPAIR WAS REMOVED AND ADDITIONAL DAMAGE WAS NOTED (BELOW AND AFT OF ORIGINAL DAMAGE). BOTH DAMAGES WILL BE REPAIRED VIA ONE REPAIR SCHEME. REPAIRED PER ERA 300413-14, REV D.

Part: SKIN — GOUGED (BS 990)

GOUGES WERE FOUND IN THE SKIN AT THE AFT EDGE OF THE C2 DOOR CUTOUT AT BS 990. THE DAMAGE WAS LOCATED BETWEEN S24 AND S24+5 INCHES. REPAIRED PER ERA 333109-14, REV A.

Part: KEEL BEAM — CRACKED (BS 870)

DURING INSPECTION OF THE LWR KEEL BEAM PER EO 4-64433-3, A CRACK WAS FOUND IN THE WEB (ONLY) JUST ABOVE THE VERT FLANGE OF THE LT SIDE BEAM. REPAIRED PER ERA 333113-14, REV B.

Part: SPAR — MISINSTALLED (NR 2 TE MIDFLAP)

NR 2 MIDFLAP / UPPER SPAR CHORD / WBL 124 / ALT FAST INSTL. DURING ACCOMPLISHMENT OF EO 4-58705-3AD, MTC WAS UNABLE TO INSTALL THE REQUIRED COLLAR AT ONE OF THE MOD FASTENER HOLES DUE TO PROXIMITY OF HOLE TO SPAR FILLET RADIUS. AUTHORIZED USE OF MINI-NUT AND RADIUS BLOCK TO FACILITATE FASTENER INSTL.

Part: SKIN — DAMAGED (RT LE FLAP)

INNER SKIN CUT TO GAIN ACCESS TO RIBS. REPAIRED SKIN PER M/M 57-54-0 FIG 80.

Part: FAIRING — CORRODED (BS 740-774)

FUSELAGE FAIRING RT AC BAY FRAME, CORROSION AROUND HINGES FOR ACCESS PANEL 3448 RBL 9 STA 740 TO 774. REMOVED PANEL 3448 DAMAGED T/E. BEGAN FABRICATING REPAIR PER M/M 53-30-1. OK TO PAINT AND INSTALL. COMPLETED FABRICATION PRIOR TO TREAT AND PAINT. INSTALLED ANGLE PER M/M 53-30-1 FIG 804. INSTALLED PANEL 3448.

Part: ANGLE — MISREPAIRED (NR 3 TE MIDFLAP)

DURING SHOP INSPECTION, THE AFT LOWER CLOSEOUT ANGLE WAS FOUND CRACKED 56 FROM IB END. THE ANGLE WAS REPAIRED PER 727 MM 57-52-0, FIG 802 BY INSTALLING A SPLICE DOUBLER AND A NEW SECTION OF ANGLE.

Part: ANGLE — REPAIRED (LT TE MIDFLAP)

DURING SHOP INSPECTION, THE AFT LOWER CLOSEOUT ANGLE WAS FOUND CRACKED 33 FROM IB END OF THE FLAP. THE ANGLE WAS REPAIRED PER MM 57-52-0, FIG 802 BY INSTALLING A DOUBLER AND SECTION OF ANGLE.

Part: RIB — CRACKED (VERT FIN)

LT STR TO RIB ATTACH FLANGE CRACKED INSIDE VERTICAL FIN AT RIB STA 179 STR 8L. FABRICATED REPAIR PER M/M 55-30-0 FIG 803. OK TO INSTALL. REPAIRED PER M/M 55-30-0 RIG 803.

Part: ANGLE — CRACKED (LT TE MIDFLAP)

DURING SHOP INSPECTION, THE LOWER AFT CLOSEOUT ANGLE WAS FOUND CRACKED 55 FROM IB END OF THE FLAP. THE ANGLE WAS REPAIRED BY INSTALLING A DOUBLER PER MM 57-52-0, FIG 802.

Part: ANGLE — MIS INSTALKLED (NR 3 TE MID FLAP)

DURING SHOP INSPECTION, THE AFT LOWER CLOSEOUT ANGLE WAS FOUND WITH FASTENERS MISSING. THE ANGLE WAS REPAIRED PER MM 57-52-0, FIG 802 BY INSTALLING A SPLICE DOUBLER AND NEW SECTION OF ANGLE.

Part: ANGLE — REPAIRED (NR 2 TE MIDFLAP)

DURING SHOP INSPECTION, THE AFT LOWER CLOSEOUT ANGLE WAS FOUND CRACKED 19 FROM THE IB END OF THE FLAP. THE ANGLE WAS REPAIRED PER MM 57-52-0, FIG 802 BY INSTALL A DOUBER AND SECTION OF ANGLE.

Part: ANGLE — REPAIRED (NR 3 TE MIDFLAP)

DURING SHOP INSPECTION, THE AFT LOWER CLOSEOUT ANGLE WAS FOUND CRACKED 34 FROM IB END. THE ANGLE WAS REPAIRED PER MM 57-52-0, FIG 802 BY INSTALLING A SPLICE DOUBLER AND NEW SECTION OF ANGLE.

Part: BUSHING — LOOSE (TE FLAPS)

NR 4 FLAPTRACK FWD MOUNT PORKCHOP FITTING BUSHING LOOSE. REMOVED FITTING, BUSHING REMOVED. CORROSION FOUND, REWORKED ON N/R 642.

Part: LIGHT — INOPERATIVE (CABIN)

AFT RT GALLEY DOOR OVERHEAD EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY, CKS GOOD.

Part: SKIN — DENTED (C2 DOORWAY)

THE FUSELAGE SKIN WAS FOUND DENTED ON THE C2 DOOR CUTOUT LOWER EDGE AT APPROXIMATELY STA 970. DAMAGED PARTS WERE THE UPPER SKIN, THE LOWER SKIN, AND THE BEAR STRAP. A CUTOUT WAS MADE THROUGH ALL THREE LAYERS WHICH MEASURED 1 BY 2. A REPAIR SCHEME WAS MADE USING A REPAIR DOUBLER AND STRAP PER ERA330583-14.

Part: STRINGER — CRACKED (BS 950)

FUSELAGE STR 29R WAS FOUND WITH A 2 INCH CRACK LOCATED AT FS 950E+2. PERFORMED STRINGER SPLICE REPAIR PER ERA 330568-14.

Part: WIRE — DAMAGED (NR 2 ENGINE)

NR 2 ENGINE OIL TEMP GUAGE PEGGED OUT HIGH DURING CLIMB AND CRUISE. PULLING THE THROTTLE TO IDLE MADE THE GUAGE FLUCTUATE BETWEEN THE YELLOW AND RED RADIAL. REMOVED AND REPLACED OIL TEMP BULB AND TEMP IND, NO HELP. REINSTALLED ORIGIND. DURING INSP, FOUND BROKEN GROUNDING WIRE. REPAIRED WIRE, RAN NR 2 ENG PER PFHB AND OIL TEMP IND NORMAL.

Part: PACKS — MALFUNCTIONED (LT/RT)

DOUBLE PACK TRIP OFF AT FL370, MIX VALVES IN MID RANGE. PACKS RECOVERED AND OPERATED NORMALLY AFTER BEING TURNED OFF AND THEN BACK ON AT FL240. PERFORMED PACK TRIP CHECK PER M/M 21-11-00, CHECKED OK.

Part: BATTERY — DISCHARGED (CABIN)

LEFT SIDE EMERGENCY LIGHT OUTSIDE AND BEHIND LEFT WING WOULD NOT ILLUMINATE STEADY. REPLACED BATTERY.

Part: LIGHT — INOPERATIVE (CABIN)

FOUND AFT STAIR OVERHEAD EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY, OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (AFT AIRSTAIR)

ON LAYOVER, FOUND EMERGENCY LIGHT ABOVE AFT AIRSTAIR INOP. RESEATED BATTERY PACK, FOUND CONTACT BROKEN ON LIGHT ASSY. REPLACED SAME.

Part: TQ BOX WEB — CRACKED (BS 1223)

FOUND ON D-2 LETTER CHECK, TORQUE BOX WEB LIGHTENING HOLE CRACKED .25 INCH, STA 1223 RT. REPAIRED PER M/M 53-11-0.

Part: DOOR PAN — CRACKED (FWD SERVICE DOOR)

FOUND ON D-2 LETTER CHECK, 3 INCH CRACK IN FWD SERVICE DOOR PAN EXTENDING FROM LOWER FWD STOP CASTING. REPAIRED PER ERA 303377-14 AND M/M 52-12-0.

Part: ANGLE — CRACKED (BS 133.8)

FOUND ON D-2 LETTER CHECK, WEB TO STRINGER ATTACH ANGLE CRACKED. VERTICAL CRAWL WAY 3RD BAY FROM TOP LT SIDE CRACK LOCATED IN STA 133.8 AT STR 9. REPAIRED PER M/M 55-30-0.

Part: RIB — CRACKED (NR 7 LE SLAT)

DURING INITIAL INSPECTION OF THE NR 7 LEADING EDGE SLAT, THE NR 11 RIB WAS FOUND TO BE CRACKED. THE RIB WAS REPAIRED PER M/M 57-54-0 FIG 804.

Part: RIB — CRACKED (NR 7 LE SLAT)

DURING INITIAL INSPECTION OF THE NR 7 LEADING EDGE SLAT, THE NR 8 RIB WAS FOUND TO BE CRACKED. THE RIB WAS REPAIRED PER M/M 57-54-0.

Part: RIB — CRACKED (NR 7 LE SLAT)

DURING SHOP INSPECTION, THE NINTH AND SIXTEENTH RIBS FROM THE OUTBOARD END OF NR 7 SLAT WERE FOUND TO BE CRACKED. THE DAMAGE WAS REPAIRED PER 727 M/M 57-54-0.

Part: RIB — CRACKED (NR 7 LE SLAT)

DURING SHOP INSPECTION, THE SECOND AND SIXTH RIBS FROM THE OUTBOARD END OF NR 7 SLAT WERE FOUND TO BE CRACKED. THE DAMAGE WAS REPAIRED PER 727 M/M 57-54-0.

Part: HEAT SHIELD — DENTED (NR 7 LE SLAT)

DURING INITIAL INSPECTION OF THE NR 7 LEADING EDGE SLAT, A DENT WAS FOUND IN THE HEAT SHIELD BETWEEN THE NR 11 AND NR 12 RIB. THE DENT WAS REPAIRED PER M/M 57-50-3 FIG 4.

Part: RIB — CRACKED (NR 7 LE SLAT)

DURING INITIAL INSPECTION OF THE NR 7 LEADING EDGE SLAT, THE NR 10 RIB WAS FOUND TO BE CRACKED. THE RIB WAS REPAIRED PER M/M 57-54-0 FIG 814.

Part: TEMP CONTROLLER — SHORTED (LT PACK)

ONCE AIRBORNE, THE LEFT PACK CONTROLLER WOULD NOT RESPOND TO MANUAL INPUTS. EVENTUALLY THE CONTROLLER GAVE OFF SOME SMOKE AND POPPED THE MAIN CONTROL CIRCUIT BREAKER. SELECTOR SHORTED INTERNALLY, REPLACED PANEL AND OPERATION NORMAL.

Part: FLOOR BEAM — CRACKED (BS 344)

FOUND ON CV 2 CHECK, CORROSION AT NUT CLIP HOLES TOP AND UNDERSIDES OF FLOOR BEAM STA 344 BETWEEN LBL 10 AND 60. REPAIRED PER SRM 53-10-8, FIG 10. INSTALL DOUBLER AND TRIPLER ON CRACKED LEG ONLY PER ENGINEER D.S.W.

Part: FLOOR BEAM — CORRODED (BS 400)

FOUND ON CV 2 CHECK, CORROSION AT FLOOR BEAM STA 400, BETWEEN RBL 33 AND 57. REPAIRED PER M/M 53-20-11.

Part: ANGLE — CRACKED (LT WING)

FOUND DURING D-1 LETTER CHECK, TORQUE BOX O/B SUPPORT ANGLE CRACKED ACTUATOR MOUNT NR 4 L/E FLAP. REPAIRED PER MM 57-20-21.

Part: TIRE — FAILED (RT MLG)

DURING CRUISE, A LOUD NOISE WAS HEARD IN CABIN. RETURNED TO ATL. THE RIGHT GEAR NR 3 TIRE HAD THE RETREAD BLOW OFF. DAMAGE OCCURED TO APU EXHAUST DUCT, GEAR DOOR RELEASE BRACKETS, L/E OF NR 3 PYLON AND RIGHT INBD AFT FLAP. WHEN WHEEL ASSEMBLY WAS CHANGED IT WAS NOTICED THAT ONLY THE RETREAD HAD SEPARATED AND THE TIRE STILL MAINTAINED PRESSURE. FOR RETURN TO SERVICE REPLACED NR 3 AND 4 WHEEL ASSEMBLIES, APU EXHAUST DUCT, L/G DOOR BRACKERS, PYLON L/E AND AFT FLAP.

Part: FIRE LOOP — SHORTED (NR 3 ENGINE)

AFTER TAKOFF, NR 3 ENGINE B FAULT DETECTOR LIGHT CAME ON. COMPLIED WITH POM, APPROXIMATELY 15 MINUTES LATER B-LOOP ILLUMINATED, SHUTDOWN ENGINE AND DISCHARGED BOTH BOTTLES. INDICATION REMAINED UNTIL SHUTDOWN AT GATE. FOUND LOWER FIRE DETECTOR LOOP SHORTED. REPLACED LOOP ASSEMBLY AND BOTTLES.

Part: CLIP — CORRODED (FS 1010)

FOUND ON CV2 CK - CORROSION ON FUSELAGE FRAME TO SKIN ATTACH CLIP FWD SIDE STA 1010 BETWEEN STR 30/29R - REPAIR - REPLACED SKIN CLIP PER M/M 53-11-0.

Part: STRINGER — CORRODED (FS 1010)

FOUND ON CV2 CK - CORROSION INSIDE STR 30 AFT OF SIDE STA 1010 JUST AFT OF FACTORY SPLICE - REPAIR - REPAIRED PER ERA 301748-14.

Part: SKIN — CORRODED (FS 1010)

DURING CORROSION VISIT INSPECTION, CORROSION WAS FOUND ON THE FUSELAGE SKIN AT STA 1010, BETWEEN STRINGER 29L AND STRINGER 30. A 2.5 BY 2.5 CUTOUT IN THE SKIN WAS REQUIRED, STRINGER 30 WAS CUT AFT OF THE FACTORY SPLICE. BOTH DAMAGE LOCATIONS WILL BE REPAIRED IN ACCORDANCE WITH B727 SRM 53-10-3 FIG 1 FOR THE STR AND B727 SRM 53-30-3 FIG 3A, FOR THE SKIN.

Part: BALANCE BOARD — CRACKED (HORIZ STAB)

FOUND ON CV-2 CHECK, .8125 CRACK AT LT INBD BALANCE BOARD ACCESS PANEL 9114. REPAIRED AS PER 55-10-3 FIG 3.

Part: SKIN — CORRODED (FS 700-720)

DURING CORROSION VISIT INSPECTION, THE LOWER FUSELAGE SKIN BETWEEN STA 700 TO 720 AND S-28L AND S-28R WAS FOUND TO HAVE CORROSION THAT REQUIRED A 33.0 BY 17.5 SKIN CUTOUT. THE SKIN WAS REPAIRED WITH AN EXTERNAL DOUBLER IN ACCORDANCE WITH AD 91-09-09, AND THE ASSOCIATED BAC S/B 727-53-0203 REV 2.

Part: FRAME — CRACKED (FS 720)

FOUND ON CV2 CHECK, FRAME CRACKED STA 720 5 INCHES ABOVE STRINGER 28L. REPAIRED PER SRM 53-10-4 FIG 26.

Part: SEAT TRACK — CORRODED (FS 400-420)

FOUND ON CV2 CHECK, CORROSION ON I/B SEAT TRACK RBL 24 BETWEEN STA 400 AND ST 420. REPAIRED PER SRM 53-10-5 FIG 7.

Part: FORMER — CORRODED (FS 740)

FOUND ON CV2 CHECK, CORROSION ON FORMER FWD SIDE STA 740 BETWEEN STR 28R TO 27R. REPAIRED FORMER PER M/M 53-11-0 FIG 826.

Part: CLIP — CORRODED (FS 700)

FOUND ON CV2 CHECK, CORROSION ON SKIN CLIP FWD OF STA 700 INBD OF STR 28L. REPAIRED PER M/M 53-10-0 PG 825.

Part: CLIP — CORRODED (FS 700)

FOUND ON CV2 CHECK, CORROSION ON SKIN CLIP FWD STA 700 INBD OF STR 28R W/W 257. REPAIRED PER M/M 53-11-0 PG 825.

Part: SPLICE — CORRODED (FS 480)

FOUND ON CV2 CHECK, CORROSION ON STRINGER SPLICE STR 26L AFT OF STA 480 FORMER. REPAIRED PER SRM 53-10-3 FIG. 1.

Part: WEB — CRACKED (FS 1236)

FOUND ON CV2 CHECK, TWO .25 INCH CRACKS AT LIGHTENING HOLE, RBL 20, FS 1236, AT PREVIOUS REPAIRS. REPAIRED PER M/M 53-11-0 PG 828.

Part: SEAT TRACK — CORRODED (FS 420)

FOUND ON CV2 CHECK, CORROSION STA 420, 43 RBL I/B SIDE MIDDLE RT SEAT TRACK. REPAIRED PER SRM 53-10-5 FIG 7.

Part: SLAT — CRACKED (NR 7 LE FLAP)

FOUND ON CV2 CHECK, NR 7 L/E SLAT CRACKED BELOW TAI DUCT SLAT S/N 1172. REPAIRED PER M/M 57-54-0 PAR 5A P807A.

Part: SKIN — CORRODED (FS 1010)

FOUND ON CV2 CHECK CORROSION ON SKIN OUTBD OF STR 28L, 2 AFT OF STA 1010. REPAIRED PER SRM 53-30-3 FIG. 3A,

Part: CLIP — CORRODED (FS 1070)

FOUND ON CV2 CHECK, CORROSION FWD SIDE OF SKIN CLIP STA 1070 BETWEEN STR 29L AND 28L. REPAIRED PER M/M 53-11-0.

Part: LIGHTNING HOLE — CRACKED (FS 1239)

FOUND ON CV2 CHECK, .25 INCH CRACK IN LIGHTNING HOLE, LBL 20, STA 1239, LOWER HOLE. REPAIRED AS PER M/M 53-11-0.

Part: LIGHTNING HOLE — CRACKED (FS 1236)

FOUND ON CV2 CHECK, .25 INCH CRACK IN LIGHTNING HOLE, RBL 20, FS 1236, LOWER HOLE. REPAIRED PER M/M 53-11-0.

Part: SEAT TRACK — CORRODED (FS 420-440)

FOUND ON CV2 CHECK, CORROSION ON SEAT TRACK RBL 24 RT I/B SEAT TRACK BETWEEN STA 420 AND STA 440. REPAIRED PER SRM FIG 7.

Part: CLIP — CORRODED (FS 950)

FOUND ON CV2 CHECK CORROSION ON AND UNDER SKIN CLIP FWD SIDE STA 950F BETWEEN STR 30L AND 29L. REPAIRED PER M/M 53-11-0 PG 825.

Part: RIB — CRACKED (NR 2 LE SLAT)

FOUND CRACKED RIB UPON INSPECTION ON NR 2 SLAT. REPAIRED RIB PER MM 57-54-00.

Part: ANGLE — CRACKED (FS 1263)

THERE IS A 1 INCH CRACK IN THE ANGLE OF THE FORWARD TRANSVERSE BEAM OF THE RT TORQUE BOX AT STA 1263. REPAIRED PER S/B 53-0129. DAMAGE FOUND AT LETTER CHECK.

Part: SPAR — CRACKED (RT ELEV)

DURING INSPECTION, THE RIGHT ELEVATOR REAR SPAR WAS FOUND TO HAVE A CRACK EMANATING .1250 INCH FROM THE INBD SIDE OF THE SHEAR PLATE AT THE SECOND FROM THE OUTBD TAB HINGE FITTING TO REAR SPAR ATTACHMENT. THE CRACK WAS STOP DRILLED IN ACCORDANCE WITH B727 S/B 55-087, THE CRACK WAS STOP DRILLED AND SET UP FOR REPETITIVE INSPECTION AND PERMANENT REPAIR.

Part: WEB — CRACKED (FS 1240)

FOUND ON C2 LETTER CHECK, TWO .25 INCH CRACKS UPPER LIGHTENING HOLE STA 1240R - AFT STAIRWELL AREA, REPAIRED PER 53-11-0 NR 15.

Part: FORMER — CRACKED (AFT FUS)

FOUND ON C2 LETTTR CHECK, FWD COWL TO FUSELAGE LIP DAMAGED AT 6 O'CLOCK POSITION, REPAIR AND REPLACED DOUBLER PER M/M 53-11-0 PG 801