N293WA

Part: SKIN — CRACKED (R/H VERT STAB) · airframe 62,862 hrs · 42,723 cycles

LWR END OF VERT STAB SKIN CRACKED R/H SIDE STA 1342 REPAIR PER M/M 55-30-000-8 FIG 801

Part: SPAR — CHAFED (RT WING) · airframe 62,862 hrs · 42,723 cycles

FOUND ON F1 LETTER CK, MLG AUX SPAR CHAFED AT INBD END. REPAIRED PER MM 57-43-000-8.

Part: PIN — BACKED OUT (CONNECTOR) · airframe 61,877 hrs · 42,070 cycles

AFT CARGO EMERGENCY LIGHT INOP ON CARGO DOOR. PIN PUSHED BACK IN D5024P. RESEATED PIN, CKS GOOD.

Part: DOOR FRAME — CORRODED (CARGO DOOR) · airframe 61,219 hrs · 41,613 cycles

THE INNER CHORD OF THE C2 DOOR CUTOUT AFT FRAME WAS FOUND WITH CORROSION BETWEEN STRINGERS 26R AND 27R. THE CORROSION WAS REMOVED BY TRIMMING OUT A 2 INCH SECTION OF THE CHORD ANGLE. THE CUTOUT IS LOCATED 6 INCHES INBOARD OF THE NR 6 DOOR STOP AND WAS REPAIRED WITH TWO ALUMINUM REPAIR ANGLES AND AN ALUMINUM REPAIR STRAP PER ER/A 379274-14.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 61,219 hrs · 41,613 cycles

NR 56 RT SIDE STA 913 ANGLE IS CRACKED AT MLG UPLOCK SUPPORT BOX. REPAIRED REF MM 53-11-0.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 60,865 hrs · 41,365 cycles

AFT AIRSTAIR OVERHEAD EMERGENCY LIGHT INOP AND ONE BULB INOP 2ND AFT EXIT SIGN AND 1 BULB INOP L1 DOOR EXIT SIGN. REPLACED PWR SUPPLY.

Part: SMOKE DETECTOR — INTERMITTENT (FWD LAVATORY) · airframe 60,863 hrs · 41,363 cycles

LAV SMOKE LIGHT ON S/O9 PANEL ILLUMINATED. NO SMOKE IN LAV. REPLACED DETECTOR.

Part: LIGHT — BROKEN (OVERWING EXIT) · airframe 60,418 hrs · 41,048 cycles

OVERWING EMERGENCY EXIT LIGHTS ON LOWER SIDEWALL HAS BROKEN BASE ON EACH OVERWING EXIT. REPLACED BASE AT EACH OVERWING EXIT.

Part: PUMP — INOPERATIVE (HYDRAULIC SYS) · airframe 59,816 hrs · 40,627 cycles

FOUND NR 2 B SYS HYD PUMP 3 PHASE C/B A PHASE LUG BURNT NEARLY THROUGH. CHECKED PWR AT PUMP CONNECTOR AND A PHASE READ 19 VOLTS. LUG WAS BURNT AND CASE MELTED. ALSO, THE WIRE INSULATION WAS BURNT. REPLACED NR 2 B PUMP, REPLACED C/B 823 AND RE-TERMINATED LUG WIRE END. CHECKS GOOD.

Part: ACTUATOR — INOPERATIVE (NR 6 LE FLAP) · airframe 59,775 hrs · 40,598 cycles

NR 6 L/E FLAP WOULD NOT RETRACT ON CLIMB OUT. SYS NORMAL AFTER ACTUATOR REPLACEMENT.

Part: SPLICE — CORRODED (STRINGER) · airframe 59,664 hrs · 40,522 cycles

FOUND DURING MV2 CORROSION VISIT, CORROSION ON STRINGER 29 LT STRINGER SPLICE REPAIR DOUBLER STA 978 O/B SIDE AND STA 970 I/B (MARKED). REPLACED EXISTING REPAIR SPLICE ANGLES PER SRM 53-10-11D FIG 802D.

Part: BRACKET — CRACKED (NR 7 SLAT) · airframe 59,664 hrs · 40,522 cycles

FOUND AT MV2 CHECK, NR 7 SLAT ACTUATOR O/B MOUNT BRACKET CRACKED AT LWR END. REPAIR PER M/M 57-42-0.

Part: ANGLE — CRACKED (NR 8 LE SLAT) · airframe 59,664 hrs · 40,522 cycles

FOUND DURING MV2 CORROSION VISIT, LOWER COVE SKIN ATTACH ANGLE CRACKED ON NR 8 SLAT AT O/B STOP PAD. REPAIRED PER M/M 57-54-0 FIG 812. NR 8 L/E SLAT (S/N BN 390).

Part: WEB — CRACKED (BS 1228)

FOUND ON D-2 LETTER CK, .5 INCH CRACK ON LT LOWER TORQUE BOX LIGHTENING HOLE FWD END STA 1228. REPAIRED PER MM 53-11-0.

Part: SKIN — CRACKED (BS 1098)

FOUND ON D-2 LETTER CK, 1 INCH CRACK LT SIDE OF STRINGER 1 STA 1098. REPAIRED PER SRM 53-30-3 FIG 3.

Part: SMOKE DETECTOR — DEFECTIVE (RT LAVATORY)

LAV SMOKE LIGHT ILLUMINATED IN FLIGHT. TWICE AT AFT LAVS. WENT OUT ON OWN FIRST TIME. HAD TO PULL CB 2ND TIME. REPLACED AFT RT LAV SMOKE DETECTOR.

Part: WIRE — FAILED (RT MLG IND)

AFTER GEAR RETRACTION RT GEAR RED AND GREEN LIGHTS REMAINED ILLUMINATED. CREW CYCLED GEAR WITH SAME RESULTS GEAR WAS VERIFIED VISUALLY TO BE UP AND LOCKED. SHORTLY AFTERWARDS BOTH LIGHTS WENT OUT THEN CAME ON INTERMITTENTLY. A/C DIVERTED TO ATL FOR MTC. REPLACED PINS 1 AND 2 IN D4660 CANNON PLUG. REPLACED WIRES FROM PLUG TO SENSOR. REPLACED LANDING GEAR ACCY BOX AS PRECAUTION. GEAR SWING CK GOOD.

Part: LINE — CRACKED (B HYD SYST)

B-SYS QTY FELL TO ZERO. FOUND HYD LINE CRACKED AT B-SYS HYD FILTER MODULE. REPLACED SAME, SERVICED QTY TO FULL. LEAK CHECK NORMAL.

Part: WEB — CRACKED (BS 1213 & 1231)

A .5 INCH CRACK TORQUE BOX VERT WEB FS 1213 RT SIDE. SEVERAL SMALL CRACKS LIGHTENING HOLE ON TORQUE BOX VERT WEB AT FS 1231 RT SIDE. REPAIRED PER MM 53-11-0 PG 833. ROUTED CRACKS PER MM 53-11-0 PG 828.

Part: BATTERY PACK — DISCHARGED (LT EMER EXIT)

LEFT AFT EMERGENCY OVERWING LIGHT INOP IN CABIN. REPLACED BATTERY RACK M1090, CKS OK.

Part: HOSE — FAILED (A-HYD SYST)

AIR TURN BACK, LOST ALL 'A' SYSTEM HYD FLUID ON CLIMB-OUT. REPLACED FLEX LINE ON LEFT ELEVATOR PCU.

Part: SKIN — CORRODED (BS 1050)

FOUND CRACK IN THE FUSELAGE SKIN AT STA 1050 JUST OUTBOARD OF STRINGER 28R. DURING REPAIR, DISCOVERED CORROSION ON INBOARD SIDE OF SKIN. REPAIRED PER DAL ER/A 304378-14.

Part: LIGHT — INOP (AIRSTAIRS)

AIRSTAIRS AREA EMERGENCY LIGHT INOP. REPLACED LIGHT.

Part: BATTERY PACK — DISCHARGED (CABIN)

RIGHT AFT OVERWING SLIDE LIGHT INOP. REPLACED BATTERY PACK AND RACK, LIGHT CHECKS NORMAL.

Part: SKIN — CRACKED (L 1 DOOR)

FOUND ON A-2 LETTER CHECK, .25 INCH CRACK IN MAIN ENTRY DOOR OUTER DOOR SKIN AT UPPER HINGE CUTOUT LOWER AFT CORNER. REPAIRED PER M/M 52-11-01.

Part: SKIN — CRACKED (PNEU DOOR CUTOUT)

FOUND ON A-2 LETTER CHECK, LOWER SKIN CRACKED .375 INCH AFT INBD CORNER OF PNEUMATIC GROUND AIR CONNECT DOOR CUTOUT. REPAIRED PER MM 53-30-0.

Part: BATTERY PACK — DISCHARGED (LT EXTERIOR)

LEFT OVER WING EXTERIOR FWD EMERG ESCAPE PATH ILLUMINATION LIGHT INOPERATIVE. REPLACED BOTH BULBS - NO HELP. REPLACED BATTERY PACK - OPERATION NOW NORMAL.

Part: SEAL — OUT OF POSITION (L1 DOOR)

AFTER TAKEOFF, EXPERIENCED EXTREMELY LOUD NOISE FROM FWD ENTRY DOOR. ACFT RTN TO BLK AT 1331. FOUND L1 DOOR LOWER HINGE FLAPPER SEAL OUT OF POSITION. CYCLE DOOR, SEAL POSITION NORMAL.

Part: BATTERY — DISCHARGED (AFT FUSELAGE)

FOUND EXTERIOR OVERWING EMERGENCY LIGHTS, AFT CARGO DOOR AND LEFT FUSELAGE INOP. RELAMPED AND REPLACED BATTERY PACK, OPERATION NORMAL.

Part: FUEL HEAT VLV — FAILED (NR 1 ENGINE)

NR 1 FUEL HEAT VALVE FAILED OPEN AFTER TAKEOFF, OIL TEMP HIT 120 DEGREES CENT, PULLED FUEL DE-ICE C/B. REPLACED FUEL HEAT VALVE, OPS CKS OK.

Part: ANGLE — CRACKED (FS 1273)

DURING LETTER CHECK IN TPA, A CRACK WAS FOUND IN THE ANGLE OF BOTH THE FWD AND AFT TRANSVERSE BEAMS OF THE RT TORQUE BOX AT FS 1273. THE DAMAGED PARTS WERE REPLACED IN ACCORDANCE WITH S/B 727-53-0129 REV 4.

Part: DOOR — MISSING (LT WING TIP)

ON ARRIVAL LGA, NAV LIGHTS ACCESS DOOR ON LT WING TIP WAS FOUND MISSING. INSTALLED NEW DOOR.

Part: SPAR — CRACKED (TE MID FLAP)

DURING SHOP INSPECTION, FOUND NR 2 MIDFLAP AFT LOWER SPAR WITH 2 CRACKS AT 53 INCHES AND 56 INCHES FROM INBD END OF FLAP. REPAIRED PER MM 57-52-20 PG 807.

Part: STRINGER — CRACKED (FIN STA 110.4)

DURING INSPECTION AT OVERHAUL, STRINGER 7R OF THE VERTICAL STABILIZER WAS FOUND CRACKED AT THE FIN STA 110.4 RIB ATTACHMENT TAB. IN ACCORDANCE WITH B727 S/B 55-0075, A REPAIR ANGLE WAS INSTALLED.

Part: STRINGER — CRACKED (VERT STAB)

DURING HMV, STR 9 LEFT INSIDE VERT STAB AT FIN STA 110 CRACKED. REPAIRED PER MM 55-30-0 PG 803 FIG 803.

Part: RIB — CRACKED (VERT STAB)

DURING HMV, FOUND RIB CHORD CRACKED AT FIN STA 110 AT STR 10 LEFT. REPAIRED PER MM 55-30-0 PG 802.

Part: ATTACH ANGLES — CRACKED (VERTICAL STAB)

FOUND DURING HMV, ATTACH ANGLE CRACKED AT NR 5 STR ABOVE NR 2 'S' DUCT INSIDE VERT STAB. REPAIRED PER SRM55-30-5 PG.1, FIG 1.

Part: STRINGER — CRACKED (VERT STAB)

FOUND DURING HMV, NR 5 STR CRACKED INSIDE VERT STAB AT STA 110.4. REPAIRED PER ERA 301113-14.

Part: PANEL — DENTED (RT LE SLAT)

DURING SHOP INSPECTION, RT WING SLAT PANEL WAS FOUND WITH DENTED UPPER SKIN. REPAIRED PER SRM 57-50-3 FIG 1.

Part: SKIN — CORRODED (FS 950)

DURING HMV, FOUND AFT B/B INNER SKIN BETWEEN STA 950/950A O/B OF STR 30 LFT CORRODED. REPAIRED PER ERA 301093-14.

Part: SKIN — CORRODED (FS 950)

BELLY SKIN INBD OF STR 29L FS 950 CORRODED. 2.8 BY 4.0 CUTOUT TO REMOVE CORROSION. A 0.040 TI-6AL-4V DOUBLER AND A 0.063 TI-6AL-4V TRIPLER INSTALLED OVER CUTOUT.

Part: COWL — WORN (NR 3 ENG NOSE)

AT HMV, NR 3 ENGINE NOSE COWL RING WAS FOUND WORN AT 3 O'CLOCK POSITION. REPAIRED PER SRM 54-10-3 FIG 3.

Part: LONGERON — CORRODED (FS 1010)

DURING HMV, FOUND SPLICE CORRODED ON STR 28R AND STR 30 AT STA 1010. REPAIRED PER SRM 53-10-11 FIG 3.

Part: FITTING — CRACKED (NR 4 LE SLAT)

AT HMV, LEFT WING NR 4 SLAT WAS FOUND WITH THE INBOARD AND OUTBOARD SLAT ACTUATOR FITTING SUPPORT RIB DOUBLERS CRACKED AT THE LOWER FORWARD FLANGE RADIUS. REPAIRED BY INSTALLING NEW DOUBLERS PER MM 57-54-0 PG 805.

Part: WEB — CRACKED (VENTRAL STAIR)

DURING HMV, RT VENTRAL STAIR LOWER BOX WEB CRACK. REPAIRED PER MM 53-11-0.

Part: RIB — CRACKED (NR 2 SLAT)

NR 2 SLAT RIB AND NR 3 CRACKED AT RADIUS FORM LWR RIB CAP. FABRICATED REPAIR PER MM 57-54-0 PG 806-807. FOUND DURING HMV.

Part: WEB — GOUGED (NR 7 LE SLAT)

FOUND DURING HMV, GOUGE IN WEB FWD OF ATTACH BOLT NR 7 SLAT O/B. REPAIRED PER M/M 57-54-0 PG 807.

Part: INTERCOSTAL — CORRODED (FS 600)

DURING HMV, INTERCOSTAL STA 600 CORRODED. REPAIRED PER SRM 51-10-4.

Part: LONGERON — CORRODED (FS 580)

DURING HMV, FOUND STR 28R CORRODED AT STA 580-600. REPAIRED PER SRM 53-10-3 PG 4.

Part: FLOOR BEAM — CORRODED (FS 1070)

DURING HMV, FOUND FLOOR BEAM CORRODED AT STA 1070 RT SIDE. REPAIRED PER SRM 53-10-8 PG 2A.

Part: CLIP — CORRODED (FS 1148)

DURING HMV, FOUND SKIN CLIP CORRODED STA 1148 STR 30. REPAIRED PER M/M 53-10-0 PG 825.

Part: STRINGER — CORRODED (FS 675)

AT HMV, FOUND CORROSION DAMAGE TO STRINGER 27R AT FS 675 TO FS 684. REMOVED SECTION OF DAMAGED STRINGER AND REPAIRED PER SRM 53-10-3 FIG 1. FUSELAGE SKIN WAS ALSO FOUND DAMAGED AT THIS LOCATION, CUT OUT DAMAGED SECTION AND INSTALLED DOUBLER PER SRM 53-30-3 FIG 3A.

Part: STRINGER — CORRODED (FS 1166)

DURING HMV, FOUND CORROSION ON STR 30 AFT OF STA 1166. REPAIRED STRINGER PER SRM 53-10-3 FIG 1.

Part: SUPPORT — CORRODED (FS 1166)

DURING HMV, CORROSION ON TOP HORIZ SUPPORT STA 1166 BULKHEAD AT CENTER CEILING SUPPORT STRAP. REPAIRED PER SRM 51-40-4 FIG 3.

Part: CLIP — CORRODED (FS 1148)

DURING HMV, FOUND SKIN CLIP CORRODED AT STA 1148 STR 29R-30. REPAIRED PER M/M 53-11-0 PG 8.

Part: DOOR FRAME — CRACKED (DOOR CUT OUT)

FOUND DURING HMV, RI1 DOOR OPENING FUSELAGE FRAME WAS FOUND CRACKED, LOWER END. REPAIRED PER SRM 53-10-4.

Part: SUPPORT FITTING — CORRODED (NR 4 MID FLAP)

NR 4 MID FLAP I/B CARRIAGE SUPPORT FITTING, UPPER I/B AND O/B THRUST BEARING RETAINER BOLT HOLES CORRODED. REPAIRED PER SRM 575004 FIG 14. INSTALLED BUSHINGS. DAMAGE REPAIRED DURING SHOP VISIT.

Part: SUPPORT FITTING — CORRODED (NR 4 MID FLAP)

NR 4 MID FLAP O/B CARRIAGE SUPPORT FITTING UPPER I/B THRUST BEARING RETAINER BOLT HOLE CORRODED. REPAIRED PER SRM 575004 FIG 14. INSTALLED BUSHING. DAMAGE REPAIRED DURING SHOP VISIT.

Part: RIB — CRACKED (NR 4 MID FLAP)

NR 4 MID FLAP I/B AFT RIB CRACKED AT LOWER AFT CORNER. REPAIRED PER M/M 575200 FIG 808 PAGE 817. DAMAGE REPAIRED DURING SHOP VISIT.

Part: WEB — CRACKED (VERT STAB)

STA 1303 INSIDE VERT STAB WEB CRACKED AT BOTH O/B ENDS AT FLOORLINE. FABRICATED RT AND LT DOUBLERS 2024T3 .040 AS PER SRM 53-10-4 PG 45. DAMAGE FOUND AT HMV.

Part: STRINGER — CRACKED (FS 720)

DURING HMV, FOUND STR 15R CRACKED AT RT FUS WING L/E LT BOX AFT OF FS 720A. REPAIRED PER SRM 53-10-3 FIG 2.

Part: STRINGER — CRACKED (WS 656)

DURING HMV, STRINGER MARKED NR 6 CRACKED AT WS 656.5. THE CRACK ORIGINATES AT HOLE AND RUNS O/B APPROX .5 INCH. REPAIR PER MM 57-13-0.

Part: SUPPORT FITTING — CORRODED (NR 4 MID FLAP)

DURING SHOP INSPECTION, NR 4 MID FLAP O/B SUPPORT FITTING THRUST BOREFLANGE PITTED WITH CORROSION. FLANGE WAS MACHINED PER SRM 57504 TO REMOVE PITS, NO BUSHING WAS REQUIRED, FITTING PN 65-19248-4.

Part: LE SKIN — WORN (NR 1 FOFE FLAP)

AT HMV SHOP INSPECTION, LEFT WING NR 1 FORE FLAP WAS FOUND WITH WEAR DAMAGE TO THE LEADING EDGE SKIN AT 64 INCHES FROM THE I/B END OF FLAP AND 26 INCHES TO 29 INCHES FROM THE O/B END OF FLAP. REPAIRED PER SRM 57-50-4.

Part: SKIN — WORN/HOLE (NR 1 FORE FLAP)

AT HMV SHOP INSPECTION, LEFT WING NR 1 FORE FLAP WAS REPAIRED FOR DAMAGE TO THE L/E SKIN AT 11 INCHES FROM THE INBOARD END OF FLAP AND A TIME LIMITED REPAIR WAS REPLACED AT 46 INCHES FROM THE OUTBOARD END OF FLAP. REPAIRED PER SRM 57-50-4.

Part: SKIN — WORN (NR 4 FORE FLAP)

AT HMV SHOP INSPECTION, NR 4 FORE FLAP WAS FOUND WITH WEAR DAMAGE TO LEADING EDGE SKIN AT 48 INCHES FROM OUTBOARD END OF FLAP. REPAIRED PER SRM 57-50-4 FIG 1.

Part: SKIN — DELAMINATED (NR 2 FORE FLAP)

HOLE IN LOWER SKIN, SEVERAL AREAS IN UPPER AND LOWER SKIN T/E ARE DELAMINATED. NR 2 FORE FLAP AT SHOP INSPECTION. MADE BONDED REPAIR PER 727 SRM 57-50-4.

Part: RAIL — CRACKED (NR 3 MID FLAP)

NR 3 MID FLAP WAS FOUND TO HAVE A CRACKED T/E LOWER RAIL 53 INCHES TO 57 INCHES FROM I/B END. REPAIRED PER MM 57-52-0. DAMAGE FOUND AT SHOP HMV VISIT.