N292WA

Part: ANGLE — CRACKED (NBR 7 SLAT) · airframe 63,835 hrs · 43,596 cycles

NBR 7 SLAT ANGLE CRACKED AT INBD STOP PAD ATTACH FOUND AT F1 LETTER CK REPAIRED PER MM 57-54-000-8

Part: ANGLE — CRACKED (NBR 8 SLAT) · airframe 63,835 hrs · 43,596 cycles

NBR 8 SLAT ANGLE CRACKED AT ANTIICE T DUCT CUTOUT FOUND ON F1 LETTER CHECK REPAIRED PER MM 57-54-000-8

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,761 hrs · 42,865 cycles

LEFT FWD AND AFT EMERGENCY EXIT EXTERIOR LIGHT INOP. REPLACED BATTERY PACKS.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,761 hrs · 42,865 cycles

LEFT FWD AND AFT EMERGENCY EXIT EXTERIOR LIGHTS INOP. REPLACED BATTERY PACKS.

Part: ENGINE — MALFUNCTIONED (NR 3) · airframe 62,663 hrs · 42,807 cycles

ON T/O ROLL, NR 3 ENG INSTR WERE UNSTABLE. ABORTED AT 110 KNOTS. ON INITIAL PWR APPLICATION NR 3 ENG WAS STABLE THEN PROGRESSIVELY BECAME UNSTABLE. NORMAL PWR USED. VERSA LUBE NR 3 ENG FUEL CONTROL. INSP MAIN CHIP DETECTOR, INSP INTAKE, EXH AND NO DEFECTS FOUND. RAN PFHB, ALL IND NORMAL.

Part: BALLAST — SHORTED (CABIN) · airframe 61,030 hrs · 41,698 cycles

BALLAST AT 15 ABC POPPED C/B AND EMITTED BURNING SMELL. REPLACED BALLAST. OP CKS NORMAL.

Part: WEB — CRACKED (TAIL) · airframe 60,538 hrs · 41,361 cycles

AT MIDVISIT, THE LT LWR CORNER OF 1303 WEB WAS FOUND CRACKED. DRILLED UP DOUBLER PER DRD 53-10-4 FIG 802. STOP DRILLED CRACK PER DRD 53-10-4 AND DYE CKED PER DRD 53-10-4D FIG 802, NO CRACK BEYOND STOP DRILL. OK TO INSTALL. INSTALLED DOUBLER PER DRD 53-10-4D FIG 802D.

Part: WEB — CRACKED (TAIL) · airframe 60,538 hrs · 41,361 cycles

AT MIDVISIT, THE RT LOWER CORNER OF THE 1303 WEB WAS CRACKED. DRILLED UP DOUBLER PER DRD 53-10-4D FIG 802D. STOP DRILLED CRACK PER DRD 53-10-4D AND DYE CKED PER DRD 53-10-4D FIG 802D. NO CRACK FOUND BEYOND DOUBLER HOLE. OK TO INSTALL. INSTALLED DOUBLER PER DRD 53-10-4D FIG 802D.

Part: RIB — CRACKED (NR 7 SLAT) · airframe 60,538 hrs · 41,361 cycles

RIB CRACKED NR 7 SLAT O/B RIB AT ACTUATOR ATTACH POINT W/W NRC 342. FABRICATED DOUBLER PER 727 MM 57-54-0 FIG 804 OK TO INSTALL DOUBLER. INSTALLED DOUBLER PER 727 MM 57-54-0 FIG 804. OK TO INSTALL PANEL. INSTALLED COVE PANEL. REMOVED AND INSTALLED ON RC 636.

Part: RIB — CRACKED (NR 7 SLAT) · airframe 60,538 hrs · 41,361 cycles

AT MV2 FOUND RW RIB CRACKED NR 7 SLAT I/B RIB AT ACTUATOR ATTACH POINT. FABBD DBLR PER MM 727-57-54-0 FIG 804. INSTALLED DBLR PER MM 57-54-0 FIG 804.

Part: RIB — CRACKED (NR 7 SLAT) · airframe 60,538 hrs · 41,361 cycles

AT MV2, RIB CRACKED NR 7 SLAT O/B RIB AT ACTUATOR ATTACH POINT. FABBED DBLR PER 727 MM 57-54-0 FIG 804, INSTALLED DBLR PER 727 MM 57-54-0 FIG 804, INSTALLED COVER PNL ON R/C 636.

Part: RIB — CRACKED (NR 7 SLAT) · airframe 60,538 hrs · 41,361 cycles

RIB-CRACKED NR 7 SLAT I/B RIB AT ACTUATOR ATTACH POINT W/W NRC 303. FABRICATED DOUBLER PER MM 727-57-54-0 FIG 804. OK TO INSTALL DOUBLER. INSTALLED DOUBLER PER 727 MM 57-54-0 FIG 804. REMOVED AND INSTALLED ON RC 636.

Part: RIB — CRACKED (NR 6 SLAT) · airframe 60,538 hrs · 41,361 cycles

AT MV2 FOUND RW RIB CRACKED NR 6 L/E SLAT, I/B RIB AT ACTUATOR ATTACH POINT. REMOVED PREV REPAIR AND FABBD REPLACEMENT DBLR PER MM 51-540 FIG 804. REPAIRED PER CMM 57-54-0 FIG 804, INSTALLED AND REMOVED ON R/C 634.

Part: LIGHT — FAILED (CABIN) · airframe 60,111 hrs · 41,082 cycles

AFT AIRSTAIR OVERHEAD EMERGENCY LIGHT WILL NOT LIGHT. REPLACED LIGHT ASSY, OP CKS GOOD.

Part: O-RING — LEAKING (NR 3 ENGINE)

NR 3 ENGINE FLAMED OUT ON APPROACH AT 6000 FEET. AT LEVEL OFF 6000 FEET DURING FINAL APPROACH SEGMENT NR 3 INSTRUMENTS INDICATED THE FOLLOWING FUEL FLOW 0 / 35 PERCENT N2 / EPR0 / N1 ZERO / NORMAL OIL PRESS, NORMAL OIL TEMP / THROTTLE MOVEMENT, NO EFFECT / NR 3 GEN LIGHT CAME ON APPROXIMENTLY 3-5 MINUTES AFTER INDICATIONS. TROUBLESHOT PER M/M, FOUND BAD O-RING ON FUEL CONTROL CONDENSATION TRAP BOWL. PERFORMED ENGINE RUN PER PREFLIGHT HANDBOOK, CHECKS OUT GOOD.

Part: LIGHT — INOP (CABIN)

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

Part: FITTING — LOOSE (NR 1 ENGINE)

ON TAKEOFF NR 1 ENG HAD LOW OIL PRESSURE AND LOW OIL PRESSURE LIGHT. ALSO, OIL QTY DROPPED. RTO FOUND BANJO FITTING LOOSE AND TIGHTEND SAME. MTC FERRY ATL FOR ENGINE CHANGE.

Part: ACTUATOR — LEAKING (LT LE FLAP)

INFLIGHT 'A' SYS HYD QTY DECREASED TO NEAR ZERO, ACCOMPLISHED PROD IAW POM. REPLACED INBOARD KRUEGER FLAP ACTUATOR.

Part: BATTERY PACK — DISCHARGED (DOOR L2)

ON L/O, FOUND EMERGENCY EXIT LIGHT OVER DOOR L2 INOP. REPLACED BATTERY PACK, OPS CKS NORMAL.

Part: FLOORBEAM — CORRODED (BS 344)

CORROSION AT FLOORBEAM STA 344 FROM LBL 13 TO RBL 17-MARKED. REPAIRED PER SRM 53-10-8 FIG 11.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

FOUND ON LAYOVER INSP, AIRSTAIR DOOR EXIT LIGHT FLICKERING. REPLACED ASSOCIATED POWER SUPPLY.

Part: RIB — CRACKED (NR 5 LE SLAT)

FOUND ON C1 LETTER CK, L/E NOSE RIB CRACKED 1.25 INCH PAST, STOP DRILL, NR 5 SLAT ACTUATOR INBD ATTACH RIB. REPAIRED PER MM 57-54-0.

Part: WEB — CRACKED (BS 1214)

FOUND AT C1 LETTER CK, RT TORQUE BOX WEB CRACKED AT UPPER END STA 1214, REPAIRED PER M/M 53-11-0 PG 832 RT TORQUE BOX WEB CRACKED .25 INCH AT UPPER LIGHTENING HOLE STA 1225. REPAIRED PER M/M 53-11-0 PG 828.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING L/O CK, FOUND RIGHT SIDE OVERWING EXIT LIGHTS INOP. REPLACED BATTERY PACK, OPS CKS OK.

Part: BATTERY PACK — DISCHARGED (CABIN)

OVERWING EXIT SIGNS INOP ON RIGHT SIDE. REPLACED BATTERY PACK AT M1086, OPS CHECKS OK.

Part: LIGHT — INOPERATIVE (FWD GALLEY)

FWD GALLEY DOOR REMOVABLE EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT ASSY AND BATTERIES, OPS CHECKS OK.

Part: HYD PUMP — INOPERATIVE (B HYD SYST)

FLT 893 - AIR TURN BACK DUE TO B-SYSTEM HYDRAULIC WENT TO ZERO WITH LOW PRESSURE LIGHT ON. A-SYSTEM AT 2.5 GALLONS. REPLACED INBOARD B-SYSTEM HYDRAULIC PUMP AND FILTERS. REPLACED NR 5 SPOILER FILTER HOUSING PACKING. RESERVICED HYDRAULIC SYSTEM. OPS AND LEAK CHECK OK.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING INSPECTION, AFT CABIN BULLNOSE EMERGENCY LIGHT INOP. REPLACED BATT RACK, OPS NORMAL.

Part: TRANSVERSE BEAM — CRACKED (FS 1273)

THERE IS A 1 INCH CRACK IN THE ANGLE OF BOTH THE FWD AFT TRANSVERSE BEAMS OF THE RT TORQUE BOX AT FS 1273. THESE AREAS OF THE TORQUE BOX ARE THE SUBJECT OF AIRWORTHINESS DIRECTIVE 94-07-08, WHICH REQUIRES INSPECTION PER S/B 53-0129. THIS ER/A WILL REPLACE THE DAMAGED PARTS IN ACCORDANCE WITH TJE S/B.

Part: ANGLE — CRACKED (NR 2 SLAT)

FOUND ON A1 LETTER CHECK, TWO .5 INCH CRACKS AT NR 2 L/E SLAT COVE SKIN ANGLE, BELOW TIA DUCT. REPAIRED PER MM 57-50-0.

Part: STRINGER — CORRODED (FS 570)

AT HMV, STR 27 L CORRODED AT WIRE SUPPORT STA 570. REMOVED CORRODED AREA, FABRICATED REPAIR SPLICE AND FILLER AS PER B-727 SRM 53-10-3.

Part: STRINGER — CORRODED (BS 570)

STRINGER 27L CORRODED AT WIRE SUPPORT STA 570. REMOVED CORRODED AREA, FABRICATED REPAIR SPLICE AND FILLER. INSTALLED REPAIR PER SRM 53-10-3, FOUND AT HMV.

Part: RIB — CRACKED (NR 3 LE SLAT)

NR 3 SLAT RIB CRACKED, I/B OF ACTUATOR ATTACH POINT CRACKED IN RADIUS AT LOWER AFT END OF RIB. INSTALLED DOUBLER PER MM 57-54-0 PG 819. FOUND AT HMV.

Part: RIB — CRACKED (NR 6 SLAT)

ITEM: NR 6 SLAT RIB CRACKED AT RIVET FWD FLANGE OF RIB NR 7. CORRECTION: REPAIRED PER S.R.M. 57-50-03, FIG 09. DAMAGE FOUND AT HMV.

Part: SKIN — DAMAGED (NR 4 SLAT)

AT HMV, FOUND NR 4 SLAT INNER ANTI-ICE SKIN BETWEEN NR 12, NR 13 RIBS HAS HOLE. FABRICATED AND INSTALLED DOUBLER PER MM 57-54-0, FIG 803A.

Part: ANGLE — CRACKED (NR 4 SLAT)

AT HMV, FOUND NR 4 SLAT ATTACH ANGLE ABOVE NR 13 RIB CRACKED. FABRICATED AND INSTALLED DOUBLER PER MM 57-54-0, PG 807.

Part: SKIN — CRACKED (NR 6 SLAT)

NR 6 SLAT SKIN CRACKED AT TAB FOR INBD TRACK FAIRING ATTACH. INSTALLED REPAIR PER MM 57-54-0, PG 820/821. FOUND AT HMV.

Part: RIBS — CRACKED (NR 4 LE SLAT)

AT HMV, FOUND NR 4 L/E SLAT WITH RIB NR 1, 10, 13, 15 CRACKED. REPAIRED CRACKED RIBS PER MM 57-54-0.

Part: BRACKET — CRACKED (NR 2 LE FLAP)

BRACKETS CRACKED, NR 2 KRUEGER FLAP ACTUATOR, O/B SUPPORT BRACKET AND I/B SUPPORT BRACKET. DYE CHECKED, FOUND NO DISCREPANCIES PER PS 900-6-301.

Part: ANGLE — CRACKED (NR 4 SLAT)

AT HMV, NR 4 SLAT ANGLE FOR CLOSEOUT PANEL CRACKED AT FWD LOWER EDGE AT RIB NR 12 AND NR 13. REPAIRED PER MM 57-54-0.

Part: SEAT TRACK — CORRODED (BS 1070-1110)

AT HMV, SEAT TRACK CORRODED, FROM FS 1070-1110 RT IB TRACK RBL 24.5. REMOVED CORROSION PER SRM 51-10-06. REPLACED TRACK FROM FS 1070 TO 1110 PER MM 53-20-11, PG 806.

Part: LE SKIN — WORN (NR 1 FOREFLAP)

AT HMV SHOP INSPECTION, NR 1 FOREFLAP FOUND WITH A HOLE IN THE L/E 10.5 INCHES FROM I/B END. REPAIRED PER SRM 57-50-4.

Part: SKIN — HOLE (NR 1 FOREFLAP)

AT HMV SHOP INSPECTION OF NR 1 F/F, WORN AREA FOUND 11 TO 12 INCHES FORM I/B END OF FLAP. ACCOMPLISHED REPAIRS PER SRM 57-50-4.

Part: SEAT TRACK — CORRODED (FS 344)

SEAT TRACK CORRODED STA 344 RT SIDE O/B, C53-224-03. REPLACED SEAT TRACK O/B RT SIDE FROM 344 TO 360 PER SRM 53-20-11, FOUND AT HMV.

Part: FRAME — MISDRILLED (FS 761)

DURING HMV, EDGE DISTANCE COULD NOT BE MAINTAINED ON ONE OF THE FASTENER HOLES THROUGH THE FLOORBEAM UPPER CHORD AT FS 761 ON RT AND LT SIDES. FOUND DURING ACCOMPLISHMENT OF EO 4-61904-3AD. REPAIRED BY PLUGGING THE DISCREPANT HOLES AND CONTINUED EO 61904-3AD. FAA APPROVAL PER FAA ALTERNATE MEANS OF COMPLIANCE LETTER 94-120S-1376 DATED 11-30-94.

Part: SUPPORT — DAMAGED (WS 913)

LT STA 913 UPLOCK SUPPORT FRAME HAS EXISTING TEMP REPAIR. INSTALLED REPAIR PER MM 53-11-0.

Part: BUSHING — WORN (NR 5 FLAP TRACK)

AT HMV, BUSHINGS WORN IN MLG DOOR LUG ON FWD END OF NR 5 FLAP TRACK. REPAIRED PER MM 57-43-0.

Part: STRINGER — CORRODED (BS 720)

AT HMV, STR 27L CORRODED AT STA 720F PLUS 10. REPAIRED PER SRM 53-10-3.

Part: STRINGER — CRACKED (VERT STAB)

AT HMV, STRINGER CRACKED INSIDE VERT STAB STR 9R CRACKED AT RIB ATTACH HOLE LOC IN FIFTH BAY UP FROM ACCESS HOLE. REPAIRED PER MM 55-30-0 PG 803.

Part: FLOORBEAM — CORRODED (FS 1090)

AT HMV, FOUND FS 1090 CABIN FLOORBEAM CORRODED AT RBL 45. ACCOMPLISHED REPAIRS PER SRM 53-10-8.

Part: STRINGER — CRACKED (FS 686.5)

PER M/M COMPLIED WITH PREVENTIVE MODIFICATION OF UPPER STR 9 AT STA 686.5, DUE TO CRACKED STR 10 AT STA 686.5. REPAIRED PER M/M 57-13-0 FIG 807, FOUND AT HMV.

Part: SEAT TRACK — CORRODED (BS 980-1036)

AT HMV, SEAT TRACK CORRODED, RBL 45 FROM FS 980 TO FS 1036 AND RBL 55 FROM FS 1030 TO FS 1100. REPLACED SECTIONS OF TRACK PER MM 53-20-11, PG 804.

Part: SEAT TRACK — CORRODED (BS 1110-1140)

AT HMV: SEAT TRACK CORRODED STA 1110 TO STA 1140 LB 25 JUST FWD OF AFT LT LAV. SEAT TRACK CORRODED STA 1110 TO STA 1140 RBL 25 JUST FWD OF AFT RT LAV. REPLACED SECTIONS OF SEAT TRACK PER MM 53-20-11, FIG 2. TRACK PER M/M 53-20-11. 2.

Part: FLOORBEAM — CORRODED (FS 380)

FLOORBEAM CORRODED FS 380 FROM RBL 24 TO CUSP RT. REMOVED CORROSION FROM FLOORBEAM CAP PER SRM 51-10-6. FABRICATED, TREAT AND PAINT REPAIR PARTS PER SRM 53-10-8.

Part: FLOORBEAM — CORRODED (BS 380)

FLOORBEAM CAP CORRODED FS 380 FROM RBL 24 TO CUSP RT. REMOVED CORROSION FROM FLOORBEAM CAP PER SMR 51-10-6. REMOVED DAMAGED FLOORBEAM, CUT OUT NEW T-CAP, INSTALLED PER SRM 53-10-6.

Part: FLOORBEAM — CORRODED (FS 1070)

CABIN FLOORBEAM FS 1070, CORROSION AT TRANSVERSAL BEAM AND LBL 64. REPAIRED PER SRM 53-10-8, FOUND AT HMV.

Part: SEAT TRACK — CORRODED (FS 1110)

CABIN FLOOR SEAT TRACKS FS 1110, ATTACH SCREWS CORRODED AT FS 1110 AND RBL 45.5. FOUND AT HMV, ACCOMPLISHED REPAIRS PER SRM 53-20-11.

Part: SEAT TRACK — CORRODED (FS 344)

TRACK CORRODED, LT I/B SEAT TRACK AT FS 344 AND RT I/B SEAT TRACK AT FS 344. REPLACED TRACK PER SRM 51-11-6, FOUND AT HMV.

Part: MIDFLAP — CRACKED CHORD (NR 2 MIDFLAP)

AFT CHORD CRACKED AT IB AFT FLAP DRIVE ROD CUTOUT. CRACK WAS REPAIRED PER MM 57-52-0 FIG 802, BY STOP DRILLING AND INSTALLING A DOUBLER. FOUND DURING SHOP VISIT FOR NR 2 MIDFLAP.

Part: STRINGER — CRACKED (VERT STAB)

AT HMV, STRINGER CRACKED INSIDE VERTICAL STAB STR 9R CRACKED AT RIB ATTACH HOLE LOC SECOND BAY UP FROM ACCESS HOLE. REPAIRED PER MM 55-30-0 PG 803.

Part: SKIN — DENTED (AILERON)

AT HMV, FOUND DENT IN UPPER SKIN OF OUTBOARD AILERON. REPAIRED PER SRM 57-50-5.

Part: RIB — CRACKED (NR 7 SLAT)

NR 7 SLAT CRACK IN LOWER END OF AFT FLANGE ON SLAT RIB 6 FROM INBD END. INSTALLED REPAIR DOUBLERS PER MM 57-54-0. FOUND AT HMV.

Part: STRINGER — CRACKED (VERT STAB)

AT HMV, STRINGER CRACKED INSIDE VERTICAL STAB STR 7L CRACKED AT RIB ATTACH HOLE, THIRD BAY DOWN FROM ACCESS HOLE. REPAIRED PER MM 55-30-0 PG 803.

Part: SKIN — WORN (NR 1 FOREFLAP)

AT HMV SHOP INSPECTION, NR 1 FOREFLAP FOUND WITH WEAR ON L/E 17.5 INCHES FROM O/B END. REPAIRED PER SRM 57-50-4.

Part: STRINGER — CORRODED (BS 1180)

STR 22L CORRODED AT STA 1180. REMOVED DAMAGED STR AND INSTALLED REPAIR PER SRM 53-10-3.

Part: RIBS — CRACKED (NR 6 SLAT)

AT HMV, FOUND NR 6 SLAT RIBS 8, 9, 11, 14, 15, 18, 19 CRACKED. INSTALLED REPAIRS ON ALL RIBS PER MM 57-54-0, FIG 814.

Part: FLOORBEAM — CORRODED (FS 1110)

BEAM CORRODED BOTTOM SIDE OF FLOOR SUPPORT AT STA 1110 TO 1130, RBL 24 I/B AND O/B NUTPLATE HOLES. REPAIRED PER SRM 53-20-11, FOUND AT HMV.

Part: STRINGER — CRACKED (WS 686.5)

AT HMV, LT UPPER WING STR 10 CRACKED AT WING RIB CAP WS 686.5. REPAIRED PER MM 57-13-0 PG 801-805.

Part: FLOORBEAM — CORROSION (BS 1110)

CABIN FLOORBEAM CORRODED BOTTOM SIDE STA 1110, RBL 12 TO LBL 12 AT NUTPLATES. REMOVED CORROSION PER SRM 51-10-6. REMOVED DAMAGED T-CAP, FABRICATED NEW T-CAP PER SRM 53-10-8. INSTALLED REPAIR PER SRM 53-10-1.

Part: ANGLE — CRACKED (NR 7 SLAT)

AT HMV, FOUND NR 7 SLAT ANGLE CRACKED ON LWR TE IB OF TRACK. FABRICATED AND INSTALLED NEW ANGLE PER MM 57-54-0, PG 812.

Part: STRINGER — CRACKED (FS 720)

AT HMV, FOUND STR 15L CRACKED AT AFT END ON AFT SIDE OF WING ICE LIGHT HOUSING AT FS 720B PLUS 15. REPAIRED PER SRM 53-10-3.

Part: RETAINERS — CORRODED (NR 1 MIDFLAP)

NR 1 MIDFLAP, I/B THRUST BEARING RETAINER, UPPER TWO BOLT HOLES CORRODED. REPAIRED PER SRM 575004 FIG 14 AND ERA302153-14. REAMED AND INSTALLED BUSHINGS, NR CARDS 6671/7220. O/B THRUST BEARING RETAINER UPPER O/B BOLT HOLE CORRODED, REPAIRED PER SRM 575004 FIG 14. REAMED AND INSTALLED BUSHING, NR 6673. REPAIRS ACCOMPLISHED AT SHOP VISIT.

Part: ANGLE — CRACKED (NR 1 LE SLAT)

NR 1 L/E SLAT CRACKED, .25 INCH CRACK IN ANGLE ON LOWER T/E 7 INCHES FROM I/B END. REPAIRED PER MM 57-54-0, FOUND AT HMV.

Part: RIB — CRACKED (NR 5 SLAT)

NR 5 SLAT CRACKED AT LOWER END OF AFT FLANGE ON RIB 19. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER PER MM 57-54-0, PG 818 AND PG 819. FOUND AT HMV.

Part: RIB — CRACKED (NR 7 LE SLAT)

NR 7 SLAT CRACKED IN LOWER AFT CORNER OF SLAT RIB 22 INCHES IB OF OB TRACK. REPAIRED DOUBLER PER MM 57-54-0 FIG 814. FOUND AT HMV.

Part: WEB — CRACKED (BS 1263/1273)

WEB CRACKED-48 SECTION INTERIOR. CLOSE OUT WEB CRACKED AT LIGHTING HOLE. LT SIDE BETWEEN STA 1263 AND STA 1273. FABRICATED AND INSTALLED REPAIR PER MM 53-11-0, PG 802. FOUND AT HMV.

Part: PANEL — CRACKED (NR 1 LE SLAT)

AT HMV, FOUND .5 INCH CRACK IN I/B UPPER CORNER OF WEB CUTOUT FOR FWD END OF ANTI-ICE DUCT OF NR 1 SLAT PANEL. STOP DRILLED CRACK, FABRICATED DOUBLER PER M/M 57-54-0.

Part: ANGLE — CORRODED (FUSELAGE)

SUPPORT CORRODED UNDER HINGES FOR PNL 3448R. INSTALLED NEW ANGLE PER SRM 53-30-1, FOUND AT HMV.

Part: STRINGER — CORRODED (FS 615)

CORROSION ON S-26L AND SUPPORT ANGLES AT STA 615. REMOVED DAMAGED STRINGER FABRICATED NEW SECTION OF STRINGER SPLICE AND INSTALLED PER SRM 53-10-3.

Part: STRINGER — CORRODED (FS 605)

CORROSION ON S-26L AND SUPPORT ANGLES AT STA 605. FABRICATED NEW SECTION OF STRINGER AND INSTALLED PER SRM 53-10-3, FOUND AT HMV.

Part: STRINGER — CORROSION (FS 585)

CORROSION ON S-26L AND SUPPORT ANGLES O/B OF S-26L AT STA 585. FABRICATED NEW SECTION OF STRINGER AND SPLICE AND INSTALLED PER SRM 53-10-3.

Part: STRINGER — CORRODED (FS 628)

AT HMV, FOUND CORROSION DAMAGE TO STR 27R AT FS 628. REMOVED CORRODED SECTION OF STRINGER, REMOVED WEB SECTION, FABRICATED NEW SECTION AND INSTALLED PER SRM 53-10-3.

Part: STRINGER — CORRODED (FS 1030)

AT HMV, FOUND CORROSION DAMAGE TO STR 28L AT FS 1030. REMOVED CORROSION PER SRM 51-10-6, REMOVED DAMAGED STRINGER, REPAIRED PER SRM 53-10-6 AND INSTALLED.

Part: STRINGER — CORRODED (FS 1050)

STRINGER 28L CORRODED ON O/B SIDE, JUST FWD OF STA 1050. REMOVED DAMAGED SECTION OF STRINGER, FABRICATED NEW SECTION OF STRINGER AND INSTALLED PER SRM 53-10-3, FOUND AT HMV.

Part: ANGLE — CORRODED (FUSELAGE)

ANGLE CORRODED UNDER HINGES FOR PANEL 3355L. REMOVED ANGLE FABRICATED NEW, INSTALLED PER MM 53-30-1 PG 808. FOUND AT HMV.

Part: TE SKIN — DELAMINATED (NR 2 SPOILER)

THE NR 2 SPOILER PANEL T/E HAS DELAMINATED. REMOVED DAMAGED AREA, COMPLETED REPAIR PER SRM 57-50-6 REF 51-40-6, FOUND AT HMV.

Part: STRINGER — CORRODED (FS 595)

CORROSION ON S-26L AND SUPPORT ANGLES O/B OF S-26L AT STA 595. ACCOMPLISHED REPAIRS PER SRM 53-10-3.

Part: ANGLE — CORRODED (BS 846)

ANGLE CORRODED FWD SIDE STA 846 RBL 10 AND LBL 10, BELOW DELTA BEAM. REMOVED ANGLE, MANUFACTURED NEW ANGLE PER M/M 53-30-1 PG 808. FOUND AT HMV.

Part: FORMER — CRACKED (BS 1050)

FORMER CRACKED AT STA 1050 BELOW STR 25R. CUT OUT DAMAGE, INSTALLED REPAIR PER SRM 53-10-4 FIG 26, FOUND AT HMV.

Part: BUSHINGS — LOOSE (NR 4 FLAP TRACK)

AT HMV, BUSHINGS LOOSE IN MLG WING DOOR LUG ON FWD END OF NR 4 FLAP TRACK. REPAIRED PER MM 57-43-0.

Part: COWL — WORN (BS 1352)

NR 2 PYLON BS 1352 MATING SURFACE BETWEEN ENG COWLS AND AFT FUSELAGE ARE WORN AT LOWER AREAS. DRILLED, HEAT TREATED, AND INSTALLED REPAIR PER MM 53-11-0.

Part: WEB — CORRODED (FS 795-800)

WEB CORRODED, FS 795-800. INSTALLED NEW WEB PER SRM 51-40-2. FOUND AT HMV.

Part: STRINGER — CORRODED (BS 595)

CORROSION ON S-26L AND SUPPORT ANGLES O/B OF S-26L AT STA 595. REMOVED CLIPS, FABRICATED NEW SECTION OF STRINGER AND SPLICE PER SRM 53-10-3. TREATED AND PAINTED PER PS 900-3-6 NR 3. INSTALLED STRINGER SECTIONS, SPLICE AND CLIP PER SRM 53-10-3 FIG 1.

Part: SKIN — DELAMINATED (LT SPOILER)

THE NR 1 SPOILER PANEL T/E HAS DELAMINATED, FOUND AT HMV. REMOVED DAMAGED AREA, COMPLETED REPAIR PER SRM 57-50-6 REF 51-40-6.

Part: SKIN — CORRODED (FS 1050)

AT HMV, SKIN CORRODED BELOW LEVELING COMPOUND OB OF STR 28R FWD OF STA 1050. REPAIRED PER SRM 53-10-3, FIG 3.

Part: TE SKIN — DELAMINATED (NR 13 SPOILER)

AT HMV, FOUND SPOILER 13 HAS T/E SEPARATION. REMOVED DAMAGED AREA AND COOKED IN NEW CORE. COMPLETED REPAIR PER SRM 57-50-6.

Part: SKIN — DELAMINATED (SPOILER)

DURING SHOP INSPECTION, SPOILER PANEL WAS FOUND WITH DELAMINATION. REPAIRED PER SRM 57-50.

Part: SKIN — CRACKED (NR 4 SLAT)

DURING SHOP INSPECTION, FOUND NR 4 SLAT SKIN CRACKED AT MOUNT HOLE FOR THE WING FENCE. REPAIRED PER MM 57-54-0.

Part: TE FAIRING — CRACKED (NR 4 SLAT)

DURING SHOP INSPECTION, FOUND NR 4 SLAT WITH THE I/B AND O/B TRACK FAIRINGS CRACKED. REPAIRED PER MM 57-54-0.