N515DA

Part: FRAME — DAMAGED (FUSELAGE) · airframe 68,017 hrs · 51,425 cycles

THE FS 1303 FRAME INNER CHORD WAS FOUND WITH FLANGE DAMAGE FROM A HYDRAULIC CLAMP ATTACH POINT 6 INCHES ABOVE THE RT VENTRAL STAIRWELL TORQUE BOX STRUCTURE. THE DAMAGE SECTION OF FLANGE WAS TRIMMED OUT AND REPAIRED WITH AN ALUMINUM REPAIR ANGLE PER ER/A 382311-14, REV A.

Part: BATTERY — DISCHARGED (CABIN) · airframe 66,899 hrs · 50,670 cycles

R1 DOOR OVERHEAD EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY BATTERIES.

Part: START VALVE — MALFUNCTIONED (NR 1 ENGINE) · airframe 66,691 hrs · 50,525 cycles

START VALVE OPEN LIGHT FOR NR 1 ENGINE ILLUMINATED AFTER TAKEOFF. COMPLIED WITH POM PROCEDURES. START VALVE EXTINGUISHED AFTER APPROXIMATELY 3 MINUTES AT IDLE POWER AND BLEED VALVE CLOSED. NO SECONDARY INDICATIONS. ACCOMPLISHED PRECAUTIONARY SHUTDOWN FOR NR 1 ENGINE. REPLACED VALVE. ALSO REPLACED THE START VALVE PRESSURE SWITCH P/N 1G309, S/N 150.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,587 hrs · 50,446 cycles

THE FWD UPPER CORNER OF THE R1 DOOR CUTOUT WAS FOUND WITH A .5 INCH CRACK EMANATING FROM A FASTENER HOLE TO THE CUTOUT EDGE. THE CRACK WAS REMOVED WITH A 1 INCH TRIMOUT THROUGH THE SKIN AND BONDED DOUBLERS. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 380839-14, REV A.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 65,882 hrs · 49,962 cycles

RT AFT EXTERIOR EMERGENCY OVERWING EXIT LIGHT INOP. REPLACED BATTERY PACK.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 65,521 hrs · 49,712 cycles

FUSELAGE SKIN PUNCTURED AT STA 1050, IMMEDIATELY BELOW THE FUSELAGE SKIN LAP JOINT AT S-20L. THE DAMAGE WAS ROUTED OUT IN A 5.5 INCH BY 5.5 INCH CUTOUT IN THE UPPER AND LOWER FUSELAGE SKIN PANELS. CORRECTIVE ACTION: ER/A 396627-14

Part: DOOR FRAME — CRACKED (CARGO BAY) · airframe 64,972 hrs · 49,338 cycles

THE INNER CHORD OF THE FWD FRAME ON THE C1 DOOR OPENING WAS FOUND WITH A .5 INCH CRACK IN THE VERTICAL FLANGE OF THE INNER CHORD JUST ABOVE THE NR 3 DOOR STOP FITTING. THE CRACK WAS ROUTED OUT OF THE FLANGE AND REPAIRED WITH TWO ALUMINUM REPAIR ANGLES INSTALLED PER ER/A 378916-14AD. THE CRACK IS TYPICAL OF AD 99-23-13 AND BAC S/B 727-53A0219.

Part: FRAME — CHAFED (NR 2 NACELLE) · airframe 64,972 hrs · 49,338 cycles

NR 2 ENG CUTOUT FRAME LIP WORN THROUGH 9:00 POS STA 1352. REPAIRED PER MM 53-11-0 PG 801.

Part: SILL — CORRODED (FUSELAGE) · airframe 64,972 hrs · 49,338 cycles

THE LOWER DOOR SILL OF THE C2 DOOR OPENING WAS FOUND WITH CORROSION ON THE OUTER FLANGE OF THE OUTBOARD CHORD BETWEEN FS 950E & 990. CLEANUP OF THE CORROSION RESULTED IN A 4.5 INCH FLANGE TRIMOUT, A 2.5 INCH TRIMOUT AND SEVERAL BLEND LOCATIONS. THE BLENDS AND TRIMOUTS WERE REPAIRED WITH TWO EXTERNAL STEEL STRAPS PER ER/A 378743-14.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 64,972 hrs · 49,338 cycles

THE FWD FRAME OF THE C1 DOOR CUTOUT WAS FOUND WITH TWO SMALL CRACKS IN THE WEB AND ONE CRACK IN THE INNER CHORD. A .375 INCH CRACK WAS FOUND IN THE WEB BETWEEN STOPS 1 & 2. A .75 INCH CRACK WAS FOUND IN THE WEB JUST BELOW STOP NR 6. A .5 INCH CRACK WAS FOUND IN THE INNER CHORD BETWEEN STOPS 2 & 3. THE CHORD CRACK WAS REPAIRED WITH AN ALUMINUM ANGLE AND THE WEB CRACKS WITH AL DOUBLERS PER B727 SRM CH 51 & ER/A 378770-14AD.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 64,972 hrs · 49,338 cycles

SKIN SUPPORT ANGLE CORRODED FS 740 STR 27R. REPAIRED PER MM 53-11-0 PG 859.

Part: RIB — CRACKED (NR 3 SLAT) · airframe 64,972 hrs · 49,338 cycles

A 1 INCH CRACK AT NR 3 SLAT I/B NOSE RIB AT SLAT ACTUATOR ROD END BOLT. REPAIR PER M/M 57-54-0 FIG 814.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,349 hrs · 48,898 cycles

FWD OVERHEAD EXIT LIGHT INOPERATIVE. R/R BATT PACK OPS CK GOOD

Part: SKIN — CRACKED (RT ELEVATOR) · airframe 63,887 hrs · 48,597 cycles

FOUND ON D2 LETTER CHECK, 2 INCH AND .25 INCH CRACK RT ELEVATOR LOWER SKIN 12 INCHES FWD OF I/B EDGE OF TAB. REPAIRED PER SRM 55-20-3.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 63,887 hrs · 48,597 cycles

FOUND AT D-2 LETTER CHECK, STR 18A CRACKED 15 INCHES FROM AFT END, RIGHT WING. REPAIRED PER M/M 53-12-0.

Part: VALVE — DAMAGED (NR 3 ENGINE) · airframe 63,767 hrs · 48,514 cycles

AIR TURNBACK DUE TO NR 3 ENGINE START VALVE LIGHT ILLUMINATED DURING CLIMBOUT. FOUND STARTER VALVE AT FAULT. ADDITIONAL DAMAGE TO STARTER AND STARTER ADAPTOR. REPLACED STARTER VALVE STARTER AND STARTER GEARBOX ADAPTER.

Part: BATTERY PACK — DISCHARGED (EMER EXIT)

DURING L/O CHECK, FOUND R1 L1 EXT EMERG LIGHTS INOP. REPLACED BATTERY PACK, OPS CHECKS GOOD.

Part: BATTERY — DISCHARGED (CABIN)

DURING L/O CHECK, FOUND LEFT AFT OVERWING EXTERNAL EMERGENCY LIGHT INOP. REPLACED BATTERY AND CHARGER, OPS CHECKS GOOD.

Part: BATTERY — DISCHARGED (CABIN)

DURING L/O CHECK, FOUND RT FWD OVERWING EMERG LIGHT INOP. REPLACED BATTERY AND CHARGER, OPS CHECKS GOOD.

Part: FUEL CONTROL — MALFUNCTIONED (NR 1 ENGINE)

NR 1 ENGINE STARTED FLUX PLUS OR MINUS .2 EPR WITH ALL OTHER ENGINE INSTRUMENTS ALSO. REPLACED NR 1 ENGINE FUEL CONTROL RAN ENG, OPS NORMAL.

Part: DETECTOR — WORN (NR 1 ENGINE)

NR 1 ENG STRUT OVERHEAT. REPLACED S/O VALVE AND CLAMPS. FOUND OVERHEAT DETECTOR WORN. REPLACED SAME, RAN ENG AND CKS GOOD.

Part: SPAR — CRACKED (CENTER WING)

WING CENTER SECTION, REAR SPAR, WEB RBL 10.75 AND LBL 14 CRACK REPAIR. THE CENTER WING REAR SPAR WAS FOUND WITH TWO SMALL TYPICAL CRACKS NEAR THE UPPER SPAR CAP AT RBL 10.75 AND LBL 14.5. THE CRACKS WERE REMOVED WITH A .25 HOLE AND .625 SLOT RESPECTIVELY. THE CUTOUTS WERE REPAIRED WITH ALUMINUM DOUBLERS PER ER/A 367797-14AD.

Part: LIGHT — INOP (CABIN)

FOUND DURING NR 7 SERVICE CHECK, EMERGENCY FLOOR TRACK LIGHTS INOP FROM COCKPIT TO 2ND ROW OF TOURIST SEATS. REPLACED BATTERY PACK, OPERATIONAL CHECKS GOOD.

Part: LIGHT — INOP (R1 DOOR)

R-1 DOOR EMERG EXIT LIGHT INOP. REPLACED LIGHT ASSY, OPS CK NORMAL.

Part: SKIN — CORRODED (BS 680)

AN AREA OF CORROSION WAS FOUND IN THE BELLY SKIN AT FS 680 AND STR 28R. THE CORROSION WAS REMOVED WITH A SKIN CUTOUT. THE CUTOUT WAS NEAR TWO PREVIOUS REPAIRS WHICH WERE REMOVED AND ONE LARGER ALUMINUM EXTERNAL SKIN DOUBLER WAS INSTALLED PER THE GUIDELINES OF B727 SRM 53-30-3 AND S/B 727-53A203. THE REPAIR WAS DOCUMENTED PER ER/A 365455-14AD.

Part: FLOORBEAM — CORRODED (BS 344)

FOUND DURING MV1 CORROSION VISIT NRC 31, CORROSION AT CLIP NUT HOLES UPPER AND LOWER SIDE OF FLOORBEAM STA 344 BL 0 RBL 24 AREA RBL 18 TO RBL 24 WITHIN LIMITS SRM 53-10-1. AREA RBL 18 TO BL 0 WORKED ON NRC 40 SRM 53-10-8.

Part: FLOORBEAM — CORRODED (BS 344)

FOUND DURING MV1 CORROSION VISIT NRC 40, CORROSION AT FLOORBEAM STA 344 FROM BL 0 TO LBL 60. WORKED WITH NRC 31. REPAIRED PER SRM 53-10-8.

Part: RIB — CRACKED (NR 1 LE SLAT)

FOUND ON C-1 LETTER CHECK, 1.5 INCH CRACK IN I/B SLAT ACTUATOR ATTACH NOSE RIB ON NR 1 SLAT. INSTALLED DOUBLER PER M/M 57-54-0 NR 4.

Part: STIFFENER — CRACKED (LT WING)

REPLACED SPAR STIFFENER PER M/M 57-20-21.

Part: FRAME — CRACKED (BS 910)

A 1 INCH VISIBLE CRACK O/B RADIUS STA 910 FRAME. REPAIRED PER M/M 53-11-0, NR 20.

Part: FRAME — CRACKED (BS 1297)

A .25 INCH CRACK ON FRAME LIGHTENING HOLE AT STA 1297 LT. REPAIRED PER M/M 53-11-0 PG 832.

Part: ROLLER — OUT OF POSITION (RT SERVICE DOOR)

RIGHT AFT SERVICE DOOR SEAL NOT MAKING CONTACT. A/C WOULD NOT HOLD PRESSURIZATION. FOUND LOWER AFT CONER ROLLER NOT IN CAM. OPENED DOOR INSP ROLLER AND STOPS. ALL CK,D GOOD. CLOSED DOOR. OP NORMAL.

Part: WEB — CRACKED (BS 1243)

FOUND B-2 CHECK, .375 INCH CRACK AT LIGHTENING HOLE AT LT LOWER TORQUE BOX STA 1243. INSTALLED DOUBLER PER M/M 53-11-0 NR 16.

Part: SKIN — CRACKED (NR 5 LE FLAP)

FOUND DURING B-2 LETTER CHECK, 1 IN CRACK NR 5 L/E FLAP SKIN AT I/B HINGE CUTOUT. REPAIRED PER M/M 57-53-0 AND ERA 363467-14.

Part: WEB — CRACKED (BS 1243)

FOUND ON B-2 CHECK, .5 IN CRACK AT RT TORQUE BOX VERT WEB LOWER LIGHTENING HOLE STA 1243. INSTALLED DOUBLER PER M/M 53-11-0 NR 16.

Part: RELAY — INOPERATIVE (COCKPIT)

ON DESCENT FOR LANDING, EMERGENCY EXIT LIGHTS CAME ON AND STAYED ON. REPLACED R-70 CHARGER CONTROL RELAY. EXIT LIGHTS CHECKED NML.

Part: OIL TEMP BULB — MALFUNCTIONED (NR 3 ENGINE)

SHUTDOWN NR 3 ENGINE AT 1505Z DUE TO HIGH ENGINE OIL TEMP. LANDED ORD 1531Z, ALL OTHER INDICATIONS WERE NORMAL. ENGINE SHUTDOWN LESS THAN 30 MINUTES. NECESSARY TO REPLACE NR 3 ENGINE OIL TEMP BULB. INSPECTED ENGINE PER MM 72-00 PG 212L. RAN ENGINE, ALL INDICATIONS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN)

R2 SERVICE DOOR EMERGENCY LIGHT INOP. REPLACED LIGHT, CHECKS GOOD.

Part: SKIN — CRACKED (NR 6 LE SLAT)

INNER SKIN CRACKED BETWEEN RIB NR 9 AND NR 10. REPAIRED PER M/M 57-54-0, FOR NR 6 L/E SLAT.

Part: ANGLE — CRACKED (NR 7 LE SLAT)

FOUND ON A1 LETTER CHECK - REWRITE FROM N/R 50 - ANGLE CRACKED .50 INCH AT NR 7 SLAT ANTI-ICE 'T' DUCT CUTOUT - REPAIR, INSTALL DOUBLER PER M/M 57-54-0, PG 807.

Part: SKIN — DAMAGED (RT ELEVATOR)

DURING INSPECTION, RT ELEVATOR WAS FOUND WITH T/E DAMAGED AT 27 TO 63 INCHES FROM THE O/B END. REPAIRED DAMAGED UPPER SKIN PER SRM 55-20-3 FIG 2.

Part: LE SKIN — WORN (NR 1 TE MIDFLAP)

DURING SHOP INSPECTION, NR 1 MIDFLAP L/E SKIN WAS FOUND WITH WEAR DAMAGE AT THE O/B END OF FLAP. REPAIRED PER MM 57-52-0 FIG 803.

Part: ACL WIRE — SHORTED (FUSELAGE)

ON CLIMB-OUT, UPPER FUSELAGE ANTI-COLLISION LIGHT FELL OUT OF MOUNT AND CAUSED POWER WIRES TO SHORT, WITH RESULTING SPARKS AND SMOKE IN CABIN. FLT RETURNED TO CAE. FOUND DAMAGED WIRES ON LIGHT ASSEMBLY. REMOVED ASSEMBLY, SECURED WIRES, PLACED ON MCO. LIGHT ASSEMBLY WAS REPLACED, OPERATION NORMAL.

Part: SKIN — DAMAGED (NR 4 TE MIDFLAP)

DURING SHOP INSPECTION, NR 4 MID-FLAP WAS FOUND WITH WEAR DAMAGE TO LEADING EDGE SKIN, AT THE OUTBOARD 9 OF FLAP. REPAIRED PER MM 57-52-0, FIG 803.

Part: SKIN — CRACKED (NR 2 TE MIDFLAP)

DURING HMV INSPECTION, FOUND NR 2 MIDFLAP WAS FOUND TO HAVE COVE SKIN CRACKED AT I/B ACTUATOR CUTOUT. REPAIRED PER M/M 57-52-0 PAGE 819.

Part: DOUBLER — CRACKED (NR 3 TE MIDFLAP)

DURING HMV INSPECTION, THE NR 2 MIDFLAP WAS FOUND CRACKED AFT SPAR RAIL REPAIR DOUBLER AT ACTUATOR CUTOUT. REPAIRED PER M/M 57-52-0, CRACKED AT 21 INCHES AND 56 INCHES FROM I/B END.

Part: FRAME — MISDRILLED (BS 784)

WHILE ACCOMPLISHING EO 4-61904-3AD AT HMV IN ATL, 2 OVERSIZED HOLES WERE DISCOVERED IN THE RT OVERWING EXIT FRAME AT STA 784. THE DOUBLER WAS MODIFIED TO REMOVE THE TWO HOLES FROM THE MODIFICATION, IN ACCORDANCE WITH BACO TWX DAL-ATL-95-0883RR DTD 8-31-95.

Part: BEAM — CRACKED (RT HORIZ STAB TE)

THE LOWER TRAILING EDGE BEAM ON THE RT HORIZONTAL STABILIZER WAS FOUND CRACKED APPROXIMATELY 2 INCHES FROM THE OUTBOARD END OF THE BEAM. ACCOMPLISHED REPAIRS PER ERA 302395-14.

Part: BLKHD — CRACKED (BS 1303)

CRACK INSIDE VERTICAL STABILIZER AT STA 1303 BULKHEAD LOWER RT CORNER, VENTRAL WALL ABOVE S-DUCT HAS CRACK. CRACK WAS FOUND AT HMV, REPAIRED BY INSTALLING DOUBLER PER SRM 53-10-4 FIG 17.

Part: BULKHEAD — CRACKED (BS 1303)

INSIDE VENTRAL STABILIZER AT STA 1303, BULKHEAD LOWER VERTICAL WALL ABOVE S-DUCT HAS CRACK AT LT CORNER. CRACK WAS FOUND AT HMV, REPAIRED PER SRM 53-10-4 FIG 17.

Part: FRAME — MISDRILLED (FS 760/783)

DURING HMV IN ATL, SEVERAL HOLES IN THE INBOARD FRAME FLANGE WERE OVERSIZED AT FS 760.95 AND FS 783.95, IN BOTH RT AND LT SIDE WHILE ACCOMPLISHING EO 4-61904-3AD. THE HOLES WERE AUTHORIZED OVERSIZED PER S/B 727-53-0197 REV 2.

Part: SKIN — CREASED (RT ELEVATOR)

AT HMV, FOUND RT ELEVATOR LOWER SKIN PANEL NR 4 FROM THE I/B END WITH CREASE. REPAIRED PER SRM 55-20-3 FIG 5.

Part: ANGLE — CORRODED (BS 740-780)

ANGLE CORRODED, A/C BAY DOOR ATTACH TEE FROM STA 740 TO 780, CORRODED WHERE HINGES ATTACH FOR PANEL 3348L. FOUND DURING HMV AND REPAIRED PER MM 53-30-1 PG 807 TO 808.

Part: ANGLE — CORRODED (BS 740-780)

ANGLE CORRODED, A/C BAY DOOR ATTACH TEE FROM STA 740 TO 780 CORRODED WHERE HINGES ATTACH FOR PANEL NR 3448. CORROSION WAS FOUND AT HMV, REPAIRED PER M/M 53-30-1 PG 807 AND 808.

Part: S-DUCT — CRACKED (EMPENNAGE)

FWD EDGE OF UPPER S-DUCT INNER SKIN CRACKED AT APPROX 6 O'CLOCK POSITION. REPAIRED PER SRM 54-10-3 FIG 9.

Part: ATTACH FITTING — CORRODED (NLG)

DURING HMV, FOUND NOSE LANDING GEAR LT PIVOT ATTACH POINTS CORRODED ON MATING FLANGES AND INSIDE OF HOLES. REPAIRED PER SRM 53-40-1.

Part: ATTACH FITTING — CORRODED (NLG)

DURING HMV, FOUND NOSE LANDING GEAR RT PIVOT ATTACH POINT FITTINGS CORRODED ON MATING FLANGES AND INSIDE OF HOLES. REPAIRED PER SRM 53-40-1.

Part: BRACKET — CRACKED (NR 5 LE FLAP)

DURING HMV, FOUND I/B MOUNT BRACKET CRACKED FOR THE NR 5 L/E FLAP ACTUATOR. REPAIRED PER 57-20-21.

Part: TRUNNION — CORRODED (RT MLG)

DURING HMV, FOUND RT MLG TRUNNION FITTING CORRODED INSIDE HOLES. REPAIRED PER M/M 57-43-0.

Part: STRINGER — CRACKED (WS 686)

DURING HMV, FOUND STRINGER CRACKED RT WING STA 686 FWD STRINGER. REPAIRED PER M/M 57-13-0 PG 808.

Part: TRUNNION — CRACKED (NR 6 FLAP)

DURING HMV, FOUND I/B TRUNNION MOUNT BRACKET CRACKED ON NR 6 FLAP ACTUATOR. REPAIRED PER M/M 57-20-21.

Part: ANGLE — CRACKED (LT SPOILER)

AT HMV, FOUND ANGLE CRACKED INBD LWR CORNER OF INBD GRND SPOILER MOUNT BOX. REPAIRED PER MM 57-55-0 PG 805.

Part: BUSHING — MISALIGNED (NR 4 FLAP TRACK)

AT HMV, FOUND LT FITTING FOR NR 4 FLAP TRACK MISALIGNED. REPLACED BUSHING PER MM 57-42-0 PG 814.

Part: BULKHEAD — FASTENER SUB (BS 1183)

WHILE ACCOMPLISHING EO 4-40130-3AD, AFT ENTRY DOORWAY AND BODY STATION 1183 BULKHEAD REINFORCEMENT, SEVERAL FASTENERS CALLED FOR BY THE DRAWING, COULD NOT BE INSTALLED DUE TO FRAME INTERFERENCE. THESE FASTENERS WILL BE SUBSTITUTED TO FACILITATE THE MODIFICATION, APPROVAL PER DL ERA 302368-14AD.

Part: BRACKET — CRACKED (LT LE FLAP)

NR 2 KRUEGER FLAP ACTUATOR BRACKET CRACKED AT RADIUS. REPAIRED PER 57-20-21 PG 811. FOUND AT HMV.

Part: STRINGER — CRACKED (WS 686.5)

LT WING UPPER STR TO RIB WS 686.5 STR NR 10 CRACKED. REPAIRED PER MM 57-13-0 PG 802. FOUND AT HMV.

Part: S-DUCT — CRACKED (CTR ENGINE)

INNER SKIN OF THE FWD SECTION OF S-DUCT IS BENT AND CRACKED AT APPROX 12 O'CLOCK POSITION. REPAIRED PER SRM 54-10-3.

Part: STRINGER — CRACKED (WS 686.5)

LT WING UPPER STRINGER TO RIB STA 686.5 STR NR 13 CRACK INDICATION HFEC. REPAIRED PER MM 57-13-0 PG 808. FOUND AT HMV.

Part: FRAME — CRACKED (L2 DOOR)

DURING HMV, FOUND L2 DR FRAME CRACKED IN LWR RADIUS OF UPPER HINGE CUTOUT. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 52-40-2.

Part: TRUNNION — CORRODED (LT MLG)

AT HMV, LEFT MLG FWD TRUNNION FTG CORRODED IN HOLES. REWORKED PER MM 57-43-0 AND PS 900-4 NR 5.

Part: ANGLE — CRACKED (LT SPOILER)

I/B LWR CORNER OF I/B GROUND SPOILER MOUNT BOX, ANGLE IS CRACKED. REPAIRED PER MM 57-55-0 PG 805.

Part: INLET — CRACKED (NR 2 ENGINE)

DURING HMV, FOUND NR 2 INLET DUCT, DOGHOUSE CRACKED AT THE 12 O'CLOCK POSITION. REPAIRED PER SRM 54-10-3 FIG 13.

Part: RIB — CRACKED (VERT STAB)

CRACK INSIDE VERTICAL STABILIZER, RIGHT SIDE 4TH BAY UP, 7TH RIB FROM TOP. CRACK FOUND AT HMV, REPAIRED PER MM 53-30-0 PG 802.

Part: SPAR — CRACKED (LT TE MIDFLAP)

DURING SHOP VISIT, FOUND THE NR 2 MIDFLAP AFT SPAR RAIL CRACKED 21 INCHES AND 56 INCHES FROM I/B END OF FLAP. REPAIRED PER M/M57-52-0.

Part: FRAME — CORRODED (FS 1090)

THE UPPER LEG OF THE C-3 DOOR CUTOUT FORWARD FRAME WAS FOUND CORRODED AT STA 1090, OUTBOARD OF STRINGER 27R. THE DAMAGE WAS REMOVED AND REPAIRED PER B727 SRM 51-40-3, FIGURE 1.

Part: PANEL — CRACKED (NR 3 TE MIDFLAP)

THE INBOARD AFT PUSHROD CUT-OUT HAS A CRACK AT INBOARD AFT CORNER. REPAIRED PER M/M 57-52-0, PAGE 819. FOR NR 3 MID-FLAP PANEL DURING SHOP INSPECTION.

Part: BULKHEAD — CRACKED (FS 1183)

DURING LETTER CHECK, FOUND A .75 INCH CRACK IN FS 1183 BULKHEAD WEB AT UPPER EDGE OF HORIZONTAL STIFFENER AT WL 168 AT RBL 25. REPAIRED PER SRM 53-10-9 FIG 6.