N528DA

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,825 hrs · 45,676 cycles

R2 DOOR EMERGENCY LIGHT INOP. REPLACED LIGHT RACK ASSY.

Part: COMPENSATOR — LEAKING (CREW O2 BOTTLE) · airframe 60,736 hrs · 45,615 cycles

CREW O2 DEPLEATED IN FLIGHT GAUGE READS 150 PSI. REPLACED CREW O2 BOTTLE AND FOUND THERMAL COMPENSATOR LEAKING. REPLACED THERMAL COMPENSATOR, LEAK CKS OK.

Part: TRANSFORMER — SHORTED (COCKPIT) · airframe 60,423 hrs · 45,388 cycles

NOSE WHEEL ILLUMINATION LIGHTS INOP ON WALKAROUND. FOUND TRANSFORMER BUS NR 1 C/B BAD TRANSFORMER T50 HIGH COIL/LOW COIL SHORTED AND WIRING DAMAGED BETWEEN TRANSFORMER AND C/B C354. REPLACED CIRCUT BREAKER, TRANSFORMER AND REPLACED WIRE 455-20.

Part: LIGHT — INOPERATIVE (LT OVERWING) · airframe 59,980 hrs · 45,082 cycles

LEFT OVERWING EMERGENCY LIGHTS ARE OUT. REPLACED BATTERY PACK AND CHARGER.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 59,632 hrs · 44,835 cycles

EMERGENCY FLASHLIGHT BATTERY WEAK. REPLACED BATTERY.

Part: ANGLE — CRACKED (TE FLAP)

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

Part: SKIN — DENTED (BS 354)

THE FUSELAGE SKIN WAS FOUND DENTED AT FS 354 AT STRINGER 3R. THE DAMAGE WAS REMOVED WITH A 1.0 CUTOUT AND REPAIRED PER ERA 333754-14.

Part: SKIN — GOUGED (BS 990)

THE FUSELAGE SKIN WAS GOUGED AT FS 990 AT STRINGER 24R. REPAIRED PER ERA 333703-14 AT HMV.

Part: SKIN — CRACKED (VERT STAB)

THE LT SKIN OF THE VERTICAL STABLIZER WAS DAMAGED RESULTING IN A 1.2 X 1.2 CUTOUT BETWEEN STRINGERS 7 AND 8 AT FIN STATION 204. REPAIRED PER ERA 333721-14 AT HMV.

Part: APU — INOP (WHEE WELL)

DURING HMV CK WORKING MCO 127703001, APU QUIT AT GATE BEFORE PUSHBACK. DURING T/S AND JIC OP 6009 FOUND APU FIRE TEST INOP. ALSO, FOUND FIRE LOOP BROKEN WITH APPARENT HIGH HEAT INDICATION AND SOOT INSIDE APU SHROUD AT INNER EXHAUST DUCT CLAMP. REPLACED APU (S/N 36681).

Part: FITTING — CRACKED (NR 4 LE SLAT ACT)

NR 4 L/E SLAT I/B ACTUATOR ATTACH FITTING WAS CRACKED 3 EA LOCATION THROUGH AN EXISTING REPAIR. REPAIRED DOUBLER PER M/M 57-54-0 FIG 804. REMOVED CRACKED PLATE, REPLACED CLIP PER 51-00. OK TO INSTALL. INSTALLED REPAIR PER M/M 57-54-0 FIG 804.

Part: RIB — CRACKED (NR 5 LE SLAT)

AT HMV FOUND NR 5 SLAT ACT MOUNT O/B RIB CRACKED. REF N/R 1140 - RIB NR 11 FROM O/B FWD. STOP DRILLED CRACK AND FABBED REPAIR PER MM 57-54-0 PG 805 AND INSTALLED PER SAME.

Part: SKIN — WORN (BS 1100)

THE FUSELAGE SKIN WAS FOUND WORN AT FS 1100 AND STRINGER 1. REPAIRED PER ERA 333691-14AD.

Part: ANGLE — CRACKED (TE FLAP)

DURING SHOP INSPECTION, THE AFT LOWER SPAR ANGLE WAS FOUND CRACKED 20 FROM I/B END. THE ANGLE WAS REPAIRED BY INSTALLING A DOUBLER PER MM 57-52-0, FIG 802.

Part: RIB — CRACKED (NR 7 LE SLAT)

AT HMV, FOUND O/B RIB CRACKED ON NR 7 L/E SLAT AT ACTUATOR FITTING. REMOVED FASTENER AND DOUBLER, FABBED NEW DOUBLER PER MM 57-54-0 FIG 804, AND INSTALLED.

Part: RIB — CRACKED (NR 8 LE SLAT)

RIB CRACKED NR 8 L/E SLAT O/B RIB. FABRICATED DOUBLER, REPAIRED PER M/M 57-54-0 FIG 814.

Part: RIB — CRACKED (NR 5 LE SLAT)

RIB CRACKED 2ND FROM I/B END ON NR 5 L/E SLAT. STOP DRILLED CRACK 2ND FROM I/B RIB ON NR 5 L/E SLAT. DRILLED VP DOUBLER FOR RIB 2ND FROM I/B NR 5 L/E SLAT. TREAT AND PAINT PER P/S 900-2-5. OK INSTALLED REPAIR. INSTALLED REPAIR DOUBLER PER M/M 57-40-0 FIG 805.

Part: MOUNT — LOOSE (SPOILER)

AT HMV, FOUND NR 13 SPOILER MOUNT BOX IS LOOSE AT LOWER ATTACH BOLTS. REPAIRED PER MM 57-42-0 PG 804.

Part: BOLT — LOOSE (SPOILER)

AT HMV, FOUND NR 14 SPOILER MOUNT BOX IS LOOSE AT LOWER ATTACH BOLTS. REPAIRED PER MM 57-42-0 PG 804.

Part: BOLT — LOOSE (SPOILER)

AT HMV, FOUND RW NR 12 SPOILER MOUNT BOX I/B LOWER ATTACH BOLT HAS PLAY. REPAIRED PER MM 57-42-0 PG 804.

Part: BUSHING — WORN (NR 2 FUEL CONTL)

ON DESCENT INTO BHM, NR 2 THROTTLE RETARDED TO IDLE NR 2 ENG WENT TO HIGH POWER SETTING AND DID NOT RESPOND TO THROTTLE MOVEMENT. ACCOM PRECAUTIONARY ENG SHUTDOWN. OPENED NR 2 ENG COWLING AT GATE AND FOUND THE BUSHING ON THE FUEL CONTROL ROD WORN OUT. REPLACED ROD END BUSHING, RAN ENGINE PER PFHB, CKS GOOD.

Part: FITTING — CRACKED (NR 2 ALTIMETER)

AT 33,000 FT, THE CAPTAINS AND F/O ALTIMETERS DIFFER BY 200 FT AND F/O ALT STICKS AT 2999. REPLACED NR 2 ALT. FOUND CRACKED DISCONNECT FITTING ON NR 2 ALT. REPLACED FITTING AND PERFORMED LEAK CHECK.

Part: SPAR — GOUGED (LT WING)

INBOARD FWD LWR SIDE OF AUX SPAR GOUGED LEFT SIDE. REPAIRED PER MM 57-43-0 P 801.

Part: SKIN — CRACKED (BS 460-680)

LFEC INSPECTION OF THE STRINGER 26L SKIN LAP SPLICE INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 14 CRACKS IN 6 DIFFERENT FRAME BAYS. THE ENTIRE SKIN LAP WAS CUTOUT TO REMOVE ALL CRACKS AND REPAIRED WITH AN EXTERNAL DOUBLER PER ER/A 367077-14AD, REV B. EXISTING ADJACENT CORROSION REPAIRS WERE INCORPORATED INTO THE LAP REPAIR.

Part: SKIN — CRACKED (BS 486)

LFEC INSPECTION OF THE STRINGER 26R SKIN LAP SPLICE INDICATED A CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN NEAR FS 486. INTERNAL HFEC INSPECTION OF THE ENTIRE PANEL LENGTH CONFIRMED A SINGLE CRACK AT FS 486. THE CRACK WAS ROUTED OUT AND REPAIRED PER B727 SRM 53-30-3, FIG 5 AND DOCUMENTED PER ER/A 367069-14AD.

Part: BATTERIES — DISCHARGED (2L DOOR)

2L EMERG EXIT LIGHT INOP. REPLACED BATTERIES, OPS CHECK GOOD.

Part: RIB — CRACKED (NR 4 LE SLAT)

FOUND ON L/O CK, NR 4 SLAT O/B ACTUATOR ATTACH RIB CRACKED AT FWD END. REPAIRED PER MM 57-54-0.

Part: DOOR — DEPARTED (NLG)

NOSE GEAR DOORS TORN FROM ACFT ON GEAR RETRACTION. REPLACED DOORS. REPAIRED NR 2 AND NR 3 SLATS. REPAIRED HOLE IN FUSELAGE. REPLACED CUT TIRE.

Part: STIFFENER — CRACKED (LE SPAR)

FOUND ON F1 LETTER CK, NR 6 SLAT O/B TRACK O/B SPAR STIFFENER CRACKED. REPAIRED PER MM 57-20-21.

Part: SPAR WEB — CRACKED (CENTER WING)

THE CENTER WING REAR SPAR WEB WAS FOUND WITH 5 CRACKS NEAR UPPER SPAR CAP. THE CRACKS ARE TYPICAL OF THOSE IN BAC S/B 727-57A0182. THE SPAR WEB WAS MODIFIED PER THE S/B WITH A CHANGE TO THE REPAIR AT RBL 20 WHERE A PREVIOUS LOCAL REPAIR WAS INSTALLED. THE REPAIR/MODIFICATION WAS ACCOMPLISHED PERER/A 365428-14AD.

Part: BEAM — CHAFED (RT MLG SUPPORT)

FOUND ON E2 LETTER CK, AFT SIDE OF MLG STRUT CHAFING FWD SIDE OF WALKING BEAM. REPAIRED PER MM 57-43-0.

Part: RIB — CRACKED (VERT STAB)

VERTICAL STAB RIB CHORD CRACKED AT FASTENER HOLE, FIN STA 157.2 AND STR 9 RT, FOUND ON E-2 LETTER CHECK. INSTALLED DOUBLER PER M/M 55-30-3 NR 2.

Part: SKIN — DAMAGED (RT TE FLAP)

COVE SKIN PANEL CUTOUT CRACKED 37 FROM I/B END. REPAIRED PER M/M 57-52-0 FIG 809.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY LIGHT BATTERY PACK POWER SUPPLY WILL NOT CHARGE. REPLACED BATTERY PACK.

Part: SKIN — CORROSION (BS 970)

THE AFT CARGO BELLY SKIN WAS FOUND CORRODED FWD OF STA 970 AND JUST O/B OF STR 28-R. THE CUTOUT REMOVING THE SKIN MEASURED 3.5(F/A) BY 3.25 (CIRC). REPAIRED PER ERA 330753-14 REV. A.

Part: STRINGER — CRACKED (BS 960)

STRINGER 29L WAS FOUND CRACKED AND CORRODED AT APPROXIMATELY STA 970. THERE WAS AN EXISTING SPLICE AT STATION 980 WHICH HAD BEEN ACCOMPLISHED BY ER/A 258938-14.

Part: RIB — CRACKED (ELEVATOR)

AT MV2, FOUND RIB CRACKED. THE LOWER SKIN AT ELEV STA 99.79 TO 136.50 HAS A BUBBLE RIB CRACKED ON O/B END. REPAIRED PER SRM 55-20-3 FIG 3.

Part: WEB — CRACKED (VERT STAB)

WEB CRACKED PAST STOP DRILL AT STA 1303 LT SIDE. INSIDE VERT STAB. REPAIRED PER SRM 53-10-4 FIG 17.

Part: BLKHD STIFFENER — CRACKED (BS 1183)

TWO CRACKS WERE FOUND IN THE VERTICAL STIFFENER AT RBL 36.83 ON THE FORWARD SIDE OF THE BS 1183 BULKHEAD. THE CRACKS ARE APPROX 1.75 AND 1 LONG AND ARE LOCATED AT APPROX WL 237 IN THE IB AND OB RADIUS, RESPECTIVELY, OF THE AFT CHORD. THIS AREA IS ADDRESSED IN EO 4-59821-3, WHICH INCORPORATES S.B. 727-53-0192. AT THIS TIME, THE BEAM WILL BE REPAIRED PER THE RELEVANT OPERATIONS OF E.O. 4-59821-3 WITHOUT ACCOMPLISHING THE MODIFICATION OF THE LBL 26.83 VERTICAL BEAM OR THE LBL 36.83 VERTICAL BEAM.

Part: WEB — CRACKED (RT VERT STAB)

WEB CRACKED PAST STOP DRILL AT STA 1303 RT SIDE INSIDE VERT STAB. REPAIRED PER SRM 53-10-4 FIG 17.

Part: FITTING — CORRODED (RT MLG TRUNNION)

RT MLG FWD TRUNNION FITTING IS CORRODED. REPAIRED PER M/M 57-42-0 PG 806-814.

Part: FITTING — CORRODED (LT MLG TRUNNION)

LT MLG FWD TRUNNION PORK CHOP FITTING IS CORRODED. REPAIRED PER M/M 57-42-0 PG 806-814.

Part: WEB — CRACKED (BS 1223)

WEB CRACKED, VENTRAL STAIR LT TORQUE BOX WEB CRACKED AT TOP RIVET ROW AFT OF STA 1223. REPAIRED PER M/M 53-10-0 PG 832.

Part: WEB — CRACKED (NR 3 LE FLAP)

AT MV2, FOUND WEB CRACKED .5 ON NR 3 AT INBD STOP CUTOUT. STOP DRILLED CRACK AND MADE DOUBLER PER MM 57-54-0 FIG 810. INSTALLED DOUBLER PER MM 57-54-0 FIG 810.

Part: WEB — CRACKED (NR 5 LE SLAT)

DURING MV-2 VISIT INSPECTION FOUND CRACKED WEB IN NR 5 SLAT AT INBD SIDE OF ACTUATOR ROD END ATTACH WEB. REPAIRED PER M/M 57-54-0 FIG 804.

Part: WEB — CRACKED (NR 4 LE SLAT)

AT MV2, FOUND WEB CRACKED 1/2 PAST STOP DRILL IN NR 4 SLAT AT INBD ROD END ATTACH WEB. REMOVED ACCESS PANEL AND DYE CHECKED RIB. STOP DRILLED CRACK PER M/M 57-54-0 FIG 811. FABRICATED AND DRILLED REPAIR PARTS IAW M/M 57-54-0 FIG 804. INSTALLED DOUBLER IAW M/M 57-54-0 FIG 804.

Part: SPAR WEB — CRACKED (WING CTR SECT)

THE WING CENTER SECTION REAR SPAR WEB IS CRACKED AT RBL 20.5. THE CRACK IS 2.625 LONG IN A CHEM-MILL RADIUS JUST BELOW THE SPAR UPPER CHORD. INSTALLED DOUBLER PER FAA/DER FORM 8110-3, DER DESIGNATION SO-775, DATED 7-3-97.

Part: BATTERY PACK — DISCHARGED (CABIN)

AFT STAIRWAY EMERGENCY LIGHT INOP. REPLACED BATTERIES IN PACK. CKS NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN)

RT AFT CARGO DOOR EMER EXIT LIGHT INOP. REPLACED BATT PACK, OPS CK GOOD.

Part: STRINGER — CRACKED (VERT STAB)

STRINGER CRACKED ON VERT STAB STA 157.2 STR 4 LT. REPAIRED PER M/M 55-30-0 FIG 803.

Part: STRINGER — CRACKED (VERT STAB)

STRINGER CRACKED ON VERT STAB STR 9 STA 44 RT SIDE. REPAIRED PER M/M 55-30-0 FIG 803.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

ESCAPE PATH LIGHTING INOP BETWEEN ROWS 27 AND 35. FOUND WIRES SHORTED IN TRACK LIGHTING. SPLICED WIRES AND REPLACED BATT PACK M9027, CKS OK.

Part: SKIN — FATIGUE (R-1 DOOR CUTOUT)

THE FUSELAGE SKIN, DOUBLER, ANT TRIPLER ARE CRACKED IN THE UPPER FORWARD CORNER OF THE R-1 DOOR CUTOUT. THE CRACK IS 0.5 LONG AND RAN FROM THE EDGE OF THE CUTOUT TO A LOCAL RIVET HOLE. THE SKIN IN THE AREA IS 0.040 THICK, THE DOUBLER IS 0.025 THICK AND THE TRIPLER IS 0.020 THICK ALL THREE LAYERS ARE MANUFACTURED FROM CLAD 2024-T3 SHEET.

Part: SKIN — CRACKED (R2 DOOR CUTOUT)

FOUND ON D-1 LETTER CHECK, R-2 DOOR UPPER FWD HINGE CUTOUT CRACKED ON FUSELAGE SKIN. REPAIRED PER SRM 52-40-2.

Part: HYD MODULE — LEAKING (ELEVATOR)

ON CLIMB-OUT, ELEV FEEL DIFFERENTIAL PRESS LIGHT BEGAN TO FLICKER, HYDRAULIC PRESSURE AND QUANTITY GOOD ON ALL SYSTEMS, ABOUT 5 MINUTES LATER, THE HYDRAULIC SYSTEM-A OVERHEAT LIGHT ILLUMINATED. TURNED NR 1 PUMP BACK ON, WAS GOOD FOR ABOUT 2 MINUTES, AND LIGHT RE-ILLUMINATED WITH LOSS OF PRESSURE AND QUANTITY ALMOST INSTANTANONEOUSLY. HAD UNEVENTFUL LANDING, FOUND ELEVATOR HYDRAULIC MODULE LEAKING FROM PLUG AT COMPENSATOR. REPLACED ELEVATOR HYDRAULIC MODULE.

Part: SKIN — CRACKED (NR 2 ENGINE)

CRACKS COMING OUT OF FASTENERS, FASTENER HOLES ON LEFT AND RIGHT SIDE OF SADDLE FAIRING NR 2 INTAKE VERTICAL STAB PANEL. FOUND DURING B-2 LTR CK. REPAIRED PER SRM 54-30-0.

Part: SKIN — CORRODED (FS 480-500)

DURING CV-2 INSPECTION, THE SKIN WAS FOUND DAMAGED IN TWO PLACES ALONG STA 480 TO 500. ONE WAS FOUND AT STR 28L AND THE OTHER NEAR STR 27L. THE DAMAGE WAS REMOVED TO LEAVE TWO CUTOUTS MEASURING 17 BY 2.5 AND 16.375 BY 1.125. AN EXISTING REPAIR IS LOCATED JUST AFT AND INBD OF THE NEW CUTOUTS. THE OLD CUTOUT IS 1.5 BY .875. IN ACCORDANCE WITH B727 SRM 53-30-3 FIG 3, THE PREVIOUS REPAIR WAS REMOVED AND A DOUBLER AND TRIPLER WERE INSTALLED TO REPAIR THE NEW CUTOUTS. ALSO, STRS 27L AND 28L HAVE BEEN REPAIRED PER B727 SRM 53-10-3 FIG 1.

Part: STRINGER — CORRODED (BS 1070)

FOUND ON CV2 CHECK, CORROSION AT STR 28R, OUTBOARD SIDE JUST FORWARD OF STA 1070. REPAIR: REPAIRED PER ERA 302065-14.

Part: INTERCOSTAL — CORRODED (BS 1070)

FOUND ON CV2 CHECK, CORROSION AT SKIN FORWARD OF STA 1070 OUTBOARD STR 28R, INBOARD OF INTERCOASTAL. REPAIR: REPAIRED PER ERA 302065-14.

Part: SKIN — CRACKED (LT AFT SVC DOOR)

FOUND ON CV2 CHECK, LEFT AFT SERVICE DOOR S/N 506 HAS .75 INCH CRACK AT UPPER HINGE CUTOUT. REPAIR: REPAIRED PER SRM 52-40-2, FIG 4.

Part: FLOORBEAM — CORRODED (BS 312)

FOUND ON CV2 CHECK, CORROSION AT FLOORBEAM STA 312 LBL 25. REPAIRED AS PER ERA 302020-14.

Part: STRINGER — CORRODED (FS 1148)

FOUND ON CV2 CHECK, CORROSION AT STR 28R AFT OF STA 1148 O/B SIDE. REPAIRED AS PER SRM 53-10-3 FIG 1, IDENTIFIED AS PERMANENT REPAIR PER PS 900-5-1 NR 4.

Part: SKIN — CORRODED (BS 480-500)

FOUND ON CV2 CHECK, CORROSION ON SKIN OUTBOARD SIDE OF STR 28L BETWEEN STA 480 AND STA 500. REPAIR: REPAIRED PER ERA 302043-14.

Part: STRINGER — CORRODED (FS 1050)

FOUND ON CV2 CHECK, CORROSION AT STR 28L STA 1050. REPAIRED PER SRM 53-30-3 FIG 1, IDENTIFIED AS A PERMANENT REPAIR PER PS 900-5-1 NR 4.

Part: STRINGER — CORRODED (BS 480-500)

FOUND ON CV2 CHECK CORROSION ON OUTBOARD SIDE OF STR 28L BETWEEN STA 480-500. REPAIR: REPAIRED PER ERA 302043-14.

Part: STRINGER — CORRODED (BS 480-500)

FOUND ON CV2 CHECK, CORROSION INSIDE STR 27L BETWEEN STA 480-500. REPAIR: REPAIRED PER ERA 302043-14.

Part: FLOORBEAM — CRACKED (FS 344)

FOUND ON CV2 CHECK, FLOORBEAM CRACKED AT FLOOR PANEL SCREW HOLE STA 344 8 INCHES OUT LBL 25. REPAIRED PER SRM 53-10-8 FIG 8.

Part: FOREFLAP — CRACKED (RT WING)

FOUND ON CV2 CHECK, CRACK RIGHT WING OB FOREFLAP AT FLAP TRACK. REPAIR: REPAIRED PER SRM 57-50-4.

Part: EEL BATTERY — DISCHARGED (CABIN)

L-2 OVERHEAD EMERGENCY EXIT LIGHT INOP. REPLACED BATTERIES, OPERATION NORMAL.

Part: EEL BATTERY PACK — DISCHARGED (CABIN)

R-2 OVERHEAD EMERGENCY LIGHT INOP. REPLACED BATTERY PACK, OPERATION NORMAL.

Part: SKIN — CRACKED (NR 5 LE SLAT)

DURING THE INITIAL INSPECTION, THE NR 5 LEADING EDGE SLAT, THE AFT HOLE ON THE OUTER SKIN WHERE THE FENCE IS MOUNTED WAS FOUND TO HAVE A .5 INCH LONG CRACK BESIDE IT. THE SKIN WAS REPAIRED PER MM 57-54-0 FIG 813.

Part: ANGLE — CRACKED (NR 5 SLAT)

DURING INITIAL INSPECTION, OF THE NR 5 LEADING EDGE SLAT, THE LOWER AFT ANGLE AT THE O/B END WAS FOUND TO HAVE A CRACK. THE CRACK WAS REPAIRED PER MM 57-54-0 FIG 805A.

Part: RIB — CRACKED (NR 7 SLAT)

A CRACK IN RIB NR 13. REPAIRED PER MM 57-54-0 PG 819.

Part: SKIN — CRACKED (NR 7 SLAT)

LOWER SKIN TO RIB ATTACH ANGLE CRACKED BETWEEN RIBS NR 7 AND NR 8. REPAIRED PER SRM 57-54-0. DURING SHOP INSPECTION, OF NR 7 L/E SLAT.

Part: RIB — CRACKED (NR 7 SLAT)

A CRACK IN NR 10 RIB LOWER AFT CORNER. REPAIRED PER MM 57-54-0. ALSO, A CRACK IN NR 11 RIB LOWER FWD CORNER. REPAIRED PER MM 57-54-0. DAMAGE FOUND AT SHOP INSPECTION, OF NR 7 SLAT.

Part: SLAT — CRACKED (NR 3 LE)

INNER SKIN CRACKED AT RIVET, O/B OF O/B ACTUATOR RIB. REPAIRED PER M/M 57-54-0 FIG 803A BY INSTALLING DOUBLER. NR 3 L/E SLAT, DAMAGE FOUND AT SHOP INSPECTION.

Part: SKIN — CRACKED (NR 3 SLAT)

THE NR 3 SLAT 727, FWD EDGE OF SKIN CRACKED AT NUTPLATES ON RIB 9 AND 10. REPAIRED PER MM 57-54-0 FIG 801, DURING SHOP INSPECTION.

Part: SLAT — CRACKED (NR 3)

NR 3 SLAT, CRACK IN UPPER CORNER OF OPENING IN SPAR FOR TEE DUCT. INSTALLED DOUBLER PER M/M 57-54-0 FIG 810. FOUND DURING SHOP INSPECTION.

Part: SKIN — CRACKED (NR 3 SLAT)

THE NR 3 SLAT 727, AFT LWR SKIN CRACKED 5 INCHES FROM O/B END. REPAIRED PER MM 57-54-0 FIG 801, DURING SHOP INSPECTION.

Part: RIBS — CRACKED (NR 3 LE SLAT)

DURING SHOP INSPECTION, NR 3 L/E SLAT WAS FOUND WITH CRACKS IN L/E RIBS NR 9 AND 10. CRACKING WAS ON THE INNER SKIN OUTBOARD OF THE OUTBOARD ACTUATOR ATTACH SUPPORT RIB, CRACK IN LOWER SKIN AT 5 FROM THE OUTBOARD END OF SLAT. ALSO, A CRACK IN THE UPPER CORNER OF OPENING IN SPAR FOR THE ANTI-ICE TEE DUCT. ACCOMPLISHED REPAIRS PER MM 57-54-0.

Part: TORQUE BOX WEB — CRACKED (RT HAND)

FOUND ON LTR CK, RIGHT FWD TORQUE BOX WEB CRACKED ALONG CHORD ANGLE RIVET ROW CRACK LENGTH 1.75 INCHES TO 2.25 INCHES. CRACK AT FWD LOWER TORQUE BOX WEB EXTENDING FROM LIGHTNING HOLE. REPAIRED PER MM 53-11-0 PG 833 AND 828.

Part: FRAME — CRACKED (FS 913.5)

FOUND ON LTR CK, FRAME CRACKED STA 913.5 IN WW. REPAIRED PER MM 53-11-0 PG 834.

Part: ANGLE — CRACKED (NR 5 LE SLAT)

LOWER AFT ANGLE CRACKED 2 INCHES O/B OF O/B STOP. REPAIRED PER MM 57-54-0 FIG 812. DURING SHOP INSPECTION OF NR 5 L/E SLAT.

Part: RIB — CRACKED (NR6 SLAT R/H LE)

DURING SHOP INSPECTION, FOUND NR 6 L/E SLAT WITH L/E RIBS NR 7 AND NR 12 CRACKED. REPAIRED PER MM 57-54-0 FIG 814.

Part: RIB — CRACKED (NR6 SLAT R/H LE)

DURING SHOP INSPECTION, NR 6 L/E SLAT WAS FOUND WITH THE 2ND RIB FROM THE O/B END OF SLAT CRACKED. REPAIRED PER MM 57-54-0.

Part: RIB — CRACKED (NR 6 SLAT LE)

DURING SHOP INSPECTION, FOUND NR 6 L/E SLAT WITH L/E RIB NR 4 CRACKED. (I/B RIB OF THE O/B TRACK). REPAIRED PER MM 57-54-0 PG. 813.

Part: RIB — CRACKED (NR 6 SLAT LE)

DURING SHOP INSPECTION NR 6 L/E SLAT WAS FOUND WITH L/E RIB NR 10 CRACKED. REPAIRED PER MM 57-54-0 FIG 814.

Part: SKIN — SCRATCHED (FS 380)

DURING INSPECTION, FOUND OUTER FUSELAGE SKIN SCRATCHED BEYOND LIMITS AFT OF FORWARD ENTRY DOOR JUST BELOW FLOOR LINE AT FS 380. REPAIRED PER SRM 53-30-3.