N282WA

Part: CHARGER — INOPERATIVE (CABIN) · airframe 73,717 hrs · 43,923 cycles

FOUND ON S/C THAT FWD OVERWING LIGHTS WERE INOP.REPLACED BATTERY PACK AND CHARGER.

Part: CONTROL VALVE — FAILED (NR 2 ENGINE) · airframe 73,215 hrs · 43,585 cycles

EXPERIENCED COMPRESSOR STALL ON NR 2 ENGINE AT 20 KTS ON TAKEOFF ROLL. ABORTED TAKE OFF. REPLACED NR 2 PRBC.

Part: LIGHT — INOPERATIVE (AIRSTAIRS) · airframe 73,185 hrs · 43,566 cycles

DURING LAYOVER CHECK FOUND EMERGENCY EXIT LIGHT ASSY AT AFT AIRSTAIRS INOP. WOULD NOT ILLUMINATE DURING EMERGENCY LIGHT CHECK, OR WHEN TEST SWITCH MOVED FROM ARM TO ON. REPLACED LIGHT ASSY AND BATTERIES. OPERATIONAL CHECKS NORMAL

Part: BEAM — CRACKED (FUSELAGE) · airframe 72,878 hrs · 43,361 cycles

INSPECTION OF THE RT TORQUE BOX OF THE VENTRAL STAIRWAY OPENING PER AD 94-07-08 AND BAC SB 727-53-0129 REVEALED A .5 INCH LONG CRACK IN THE UPPER HORIZONTAL BEAM AT FS 1263. THE DAMAGED PART WAS REMOVED AND A NEW PART INSTALLED PER THE REQUIREMENTS OF THE SB AND ER/A 381245-14AD.

Part: START VALVE — MALFUNCTIONED (NR 1 ENGINE) · airframe 72,285 hrs · 42,960 cycles

AT CRUISE THE NR 1 ENG START VALVE ILLUMINATED. FOLLOWED THE POM AND SHUT DOWN ENGINE. OIL PRESSURE AT 37 PSI FOR 1 HOUR AND 10 MINUTES. REPLACED NR 1 ENG. START VALVE AND PRESSURE SWITCH RAN ENG. CK NORMAL. PERFORMED WINDMILLING INSPECTION PER M/M.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 72,157 hrs · 42,877 cycles

FOUND AFT EMERGENCY EXIT BATTERY DEAD. REPLACED BATTERY PACK.

Part: COMPRESSOR — STALLED (NR 1 ENGINE) · airframe 71,619 hrs · 42,543 cycles

NR 1 ENGINE COMPRESSOR STALLED AT 80 KNOTS ON TAKEOFF. ABORTED TAKEOFF AND RETURNED TO THE GATE. ENGINE CHANGED.

Part: BATTERY PACK — DISCHARGED (ROW 3) · airframe 70,147 hrs · 41,645 cycles

OVERHEAD EMERGENCY LIGHT AT SEAT ROW 3 INOP. REPLACED BATTERY PACK AND RACK. OPS CHECK OK.

Part: HINGE — NOISEY (PAX DOOR)

UPON LEVELING FL 260 LOUD PIERCING SQUEAL FROM FWD ENTRY DOOR. RAISED CABIN ALTITUDE, LOWERED CABIN ALT, CLIMBED A/C AND DESCENDED A/C. CABIN 5600 TO 1000 FT. A/C FL310 TO FL240. NO IMPROVEMENT. SQUEAL REMAINED. FOUND UPPER HINGE SEAL OUT OF PLACE. INSTALLED PIN IN HINGE FITTING, CKS OK.

Part: SKIN — WORN (RT TE FLAP)

COVE SKIN WORN 34 FROM INBD END, REPAIRED PER MM 57-52-0 FIG 809, ON SHOP ORDER 877885.

Part: FRAME — CRACKED (BS 783.95)

THE LT FS 783.95 OVERWING EXIT FRAME WAS FOUND CRACKED AT HMV. THE DAMAGE WAS REPAIRED PER ERA 333610-14AD.

Part: SPAR — MISDRILLED (CENTER WING)

ONE FASTENER HOLE WAS MISDRILLED AND ELONGATED IN THE WING CENTER SECTION REAR SPAR WEB AT APPROXIMATELY LBL 41 DURING THE ACCOMPLISHMENT OF A MODIFICATION TO THE WEB. THE DAMAGE WAS FOUND AT HMV AND REPAIRED PER ERA 333636-14AD.

Part: SKIN — CORRODED (BS 820)

THE WING CENTER SECTION LOWER SKIN WAS FOUND CORRODED AT FS 820 AND RBL 13. THE DAMAGE WAS REPAIRED PER ERA 333611-14ADAT HMV.

Part: SKIN — CRACKED (BS 360-481)

CRACK INDICATIONS WERE FOUND IN THE FUSELAGE SKIN LAP AT STRINGER 4L BETWEEN FS 360 AND FS 481. THE DAMAGE WAS REPAIRED PER ERA 333599-14AD AT HMV.

Part: DOUBLER — TORN (FUSELAGE)

THE AFT LAV SERVICE PANEL DOUBLER WAS FOUND TORN DURING MODIFICATION PER EO 4-69078-3AD. THE DAMAGE WAS REPAIRED PER ERA 333642-14 AT HMV.

Part: STRINGER — CRACKED (WS 304)

THE LEFT WING STRINGER 17 WAS FOUND CRACKED AT WS 304. THE DAMAGE WAS REPAIRED PER ERA 333619-14 AT HMV.

Part: TRACK — CORRODED (TE FLAP)

INB'D FLAP NR 5 FLAP TRACK, TYPICAL CORROSION AT MLG AND SPOILER BEAM ATTACH PADS AND WEAR AT FWD ATTACH LUGS, REF AD 90-07-05 AND 90-06-09. AUTHORIZED MACHINING OF ALL CORRODED AND WORN SURFACES. SPLICE PLATE REPAIR INSTALLED OVER OVERSIZED MLG BEAM ATTACH HOLES.

Part: TRACK — CORROSION (TE FLAP)

INB'D FLAP, NR 4 FLAP TRACK: TYPICAL CORROSION AT MLG AND SPOILER BEAM ATTACH PADS AND TYPICAL WEAR AT FWD ATTACH LUGS AND SPACER BLOCK BOLT HOLES, REF AD 90-07-05 AND 90-06-09. AUTHORIZED MACHINING OF ALL CORROSION AND WEAR. SPLICE PLATE REPAIR INSTALLED OVER MLG BEAM ATTACH HOLES.

Part: SKIN — CRACKED (BS 360-481)

THE FUSELAGE SKIN WAS FOUND CRACKED AT THE STRINGER 4L LAP JOINT FROM FS 360-481. THE DAMAGE WAS REPAIRED PER ERA 333599-14AD AT HMV.

Part: FRAME — CRACKED (BS 784)

THE OVERWING EXIT FRAME AT FS 784 WAS FOUND CRACKED. THIS DAMAGE WAS REPAIRED AT HMV PER ERA 333610-14.

Part: SKIN — WORN (NR 4 TE MIDFLAP)

DURING SHOP INSPECTION, THE UPPER SKIN WAS FOUND WORN AT THE OUTBOARD END LEADING EDGE. THE SKIN WAS REPAIRED PER CMM 57052-0, FIG 803, BY CUTTING OUT THE DAMAGE AND INSTALLING A DOUBLER AND FILLER.

Part: STRINGER — CRACKED (RT WING)

FOUND AT HMV, HFEC SHOWS CRACK INDICATION: R/W STR TO RIB UPPER FWD FASTENER HOLE MARKED NR 7 AT WS 601-5. CUTOUT HOLE PER MM 57-13-0, DRILLED REPAIR ANGLE PER, DISCONNECTED FUEL TRANS TUBE, INSTALLED PARTS, REINSTALLED COVER CONT N/R 1282, RESTALLED TUBE, SEALED PER MM 57-13-00.

Part: STRINGER — CRACKED (WS 629)

AT HMV2, FOUND STRINGER TO RIB CRACKED AT ATTACHMENT HOLES WS 629.0 STR NR 3 MARKED. REMOVED FUEL PROBE REMOVED CLAMPS DISCONTINUED FUEL DUMPD, DRILLED REPAIR MM 57-13-0 FIG 802. INSTALLED REPAIR PER M/M 57-13-0 PG 802, RECONTED CLAMPS AND TUBE.

Part: STRINGER — CRACKED (WS 656.5)

AT HMV2, FOUND HFEL SHOWS CRACK INDICATION WS 656.5 STRINGER TO RIB UPPER FASTENER HOLE FWD MOST RIB. STOP DRILLED CRACK, DRILLED UP REPAIR PER MM 57-13-00 FIG 804, ANGLES FWD/AFT, INSTALLED ALL EXCEPT COVER PLATE PER MM 57-13-00. REPAIRED PER MM 57-13-00 FIG 804.

Part: RIB — CRACKED (NR 7 LE SLAT)

AT HMV2, RIB CRACKED NR 7 L/E SLAT, NR 5 L/E SUPPORT RIB IS CRACKED AT UPPER LEG. REMOVED FASTENERS AND CLIPS, STOP DRILLED CRACK MM 57-54-00 FIG 809. REPAIRED PARTS PER SAME, INSTALLED DOUBLER PER 57-54-00.

Part: RIB — CRACKED (NR 7 LE SLAT)

AT HMV2, FOUND NR 4 L/E SUPPORT RIB IS CRACKED UPPER LEG. REMOVED FASTENERS AND CLIP, STOP DRILLED, FABRICATED DOUBLER REPAIR PER 57-54-00 FIG 809, AND INSTALLED PER SAME.

Part: SKIN — CRACKED (NR 5 LE SLAT)

SKIN CRACKED UNDER FENCE NR 5 SLAT. REPAIRED AS PER MM 57-54-0.

Part: ACTUATOR — LOOSE (NR 13 SPOILER)

AT HV2, FOUND NR 13 SPOILER ACTUATOR MOUNT BOX IS LOOSE AT LOWER MOUNT BOLTS 2, I/B MOUNT POINT IS MISSING SHIMS. SHIMS REPAIRED PER MM 57-42-0.

Part: ANGLE — CRACKED (RT WING)

AT HMV, FOUND RT WING REAR SPAR LWR CHORD ANGLE IS CRACKED, O/B OF NR 5 FLAP TRACK. REMOVED CRACKED SECTION, FABRICATED NEW PER MM 57-55-0, AND INSTALLED.

Part: SKIN — CRACKED (RT WING)

SKIN CRACKED AND WORN SEVERAL PLACES AT FENCE MOUNT AREA. REPAIRED PER M/M 57-54-0.

Part: SPAR — CRACKED (RT WING)

LOWER SPAR CRACKED AT NUT PLATE ON NR 11 RIB, MARKED. REPAIRED PER M/M 57-54-0.

Part: SKIN — CRACKED (BS 481-681)

FUSELAGE SKIN, FS 481-681, STRG 4R, SKIN LAP SPLICE, CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 28 CRACKS ALONG THE PANEL LENGTH. THE ENTIRE SKIN LAP SPLICE WAS CUTOUT AND REPAIRED WITH AN EXTERNAL SKIN DOUBLER PER ER/A 367751-14AD.

Part: SKIN — CRACKED (BS 440-460)

LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 & 480 INDICATED A CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED A SINGLE CRACK BETWEEN FS 440 & 460. THE CRACK WAS ROUTED OUT OF THE SKIN LAP AND AN EXTERNAL ALUMINUM DOUBLER INSTALLED PER B727 SRM 53-30-3, FIG 5 AND ER/A 367752-14AD.

Part: RIB — CRACKED (NR 5 LE SLAT ACT)

A-1 LTR CHK, NR 5 SLAT ACT NOSE RIB CRACKED O/B SIDE AT FWD RADIUS.

Part: FAN — FAILED (CARGO COMPT)

SMELL OF SMOKE NOTED IN CABIN PRIOR TO TAKEOFF. RETURNED TO GATE, GASPER FAN C/B POPPED. REPLACED GASPER FAN, OPS CKS OK. FAN HAD CAUSED SMOKE IN CABIN.

Part: WIRE — FAILED (CABIN)

A/C ESCAPE PATH LIGHTING FOUND INOP IN SEVERAL LOCATIONS. REPAIRED AND REPLACED GROUND WIRING AT THE FWD BATTERY PACK MULTI SPLICE AREA. ALL CK'S OK.

Part: SKIN — PUNCTURED (BS 530)

FUSELAGE SKIN FS 520-540, STRINGER 25L-26L, REPAIR FOR PUNCTURE. THE FUSELAGE SKIN BETWEEN FS 520 AND 540 AND BETWEEN STRINGERS 25L AND 26L WAS PUNCTURED. THE DAMAGED SKIN WAS CLEANED UP WITH A 9 BY 5 CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER B727 SRM 53-30-3 AND DOCUMENTED PER ER/A 366704-14.

Part: OIL PRESS VALVE — FAILED (NR 3 ENGINE)

ON CLIMBOUT, NR 3 ENG OIL PRESS INDICATED IN THE RED, AT IDLE OIL PRESS IN THE GREEN. ANY ATTEMPT TO GO OVER 55 PERCENT. PRESSURE WOULD CLIMB TOWARDS THE RED. REPLACED OIL PRESSURE RELIEF VALVE.

Part: CHANNEL — CRACKED (BS 1263)

THE AFT CHANNEL OF THE VENTRAL STAIRWAY TORQUE BOX AT FS 1263 WAS FOUND WITH A TYPICAL CRACK. THE DAMAGED PART WAS REMOVED AND REPLACED WITH A NEW PART PER THE REQUIREMENTS OF BAC S/B 727-53-0129 AND DOCUMENTED PER ER/A 364426-14AD.

Part: RIB — WORN (BS 1342)

HOLE WORN THROUGH LIP OF NR 2 ENGINE CUTOUT AT 9 O'CLOCK POSITION. FOUND ON LETTER CHECK F-1. INSTALLED DOUBLER PER M/M 53-11-0 PG 801.

Part: STIFFENER — CRACKED (NR 3 LE SLAT)

A 2 INCH CRACK WING L/E VERT STIFFENER AFT OF NR 3 SLAT I/B TRACK. REPAIRED PER MM 57-20-21 PG 813.

Part: WEB — CRACKED (BS 1223)

FOUND ON F1 LETTER CK, .125 INCH CRACK AT LIGHTENING HOLE IN LT TORQUE BOX VERTICLE WEB STA 1223. ROUTED OUT DAMAGED AREA PER MM 53-11-0.

Part: HEAT VALVE — FAILED (FUSELAGE)

UNABLE TO MAINTAIN CABIN PRESS ON CLIMBOUT WITH ONE PACK. ON MCO CABIN ROSE TO 7,000 FT WITH .18 DIFFERENTIAL BEFORE DESCENT TO REGAIN CONTROL. CARGO HEAT AND OUT FLOW VLV TRIED MANUALLY AS WELL. REPLACED CARGO HEAT VLV.

Part: TIE BOLT — SHEARED (STR S-3A)

THE INBOARD TENSION TIE BOLT AT THE RT S-3A WAS FOUND SHEARED. THIS PROBLEM IS THE SUBJECT OF BACO S/B 727-53-0178, REV 2. THE BOLT WAS REPLACED AND THE TENSION TIE FITTING WAS INSPECTED IN ACCORDANCE WITH THE SERVICE BULLETIN.

Part: WEB — CRACKED (FUSELAGE)

LOWER TORQUE BOX WEB CRACKED .25 INCH AT LIGHTENING HOLE STA 1223 RT. REPAIRED PER M/M 53-10-0.

Part: BRACKET — CRACKED (NR 1 LE FLAP)

FOUND ON E1 LETTER CK, NR 1 L/E FLAP ACTUATOR O/B MOUNT BRACKET CRACKED. REPAIRED PER M/M 57-20-21.

Part: LIGHT — INOPERATIVE (CABIN)

FOUND EMERGENCY EXIT LIGHT ABOVE 1L DOOR WILL NOT COME ON. REPLACED LIGHT EXIT ASSY.

Part: RIB — CRACKED (NR 4 LE SLAT)

LOWER FLANGE OF RIB NR 18 CRACKED IN RADIUS. STOP DRILLED CRACK AND REPAIRED PER SRM 57-54-0.

Part: RIB — CRACKED (LE SLAT)

LOWER AFT FLANGE DOUBLER CRACKED, UPPER FWD FLANGE CRACKED PAST STOP DRILL AND LOWER FWD FLANGE DOUBLER CRACKED. REPLACED RIB.

Part: RIB — CRACKED (NR 4 LE SLAT)

LOWER AFT FLANGE CRACKED, UPPER FLANGE CRACKED AND STOP DRILLED BUT NO DOUBLER AND FWD FLANGE HAS TEMPORARY REPAIR. REPLACED RIB.

Part: SPAR WEB — DAMAGED (NR 4 LE SLAT)

UPPER SPAR WEB FLANGE DAMAGED BY STOP DRILLING RIBS NR 11 AND NR 12. MANUFACTURED DOUBLER, REPAIRED PER SRM 57-50-3 FIG 4.

Part: VALVE — MALFUNCTIONED (RIGHT)

ON CLIMBOUT THROUGH 29,000 FT, THE CABIN CONTINUED TO CLIMB THROUGH THE PRESET 4,800 CABIN ALITITUDE. DESENCED TO 18,000 WHERE THE CABIN STABLIZED AT 10,000. PACK BLEEDS AND OUTFLOW APPEARED OK. REPLACED RT FLOW CONTROL VALVE, LEAK CKS GOOD. PRESSURIZED A/C TO 7 PSI DIFF, ALL SYS NORMAL.

Part: TRANSDUCER — FAULTY (NR 3 WHEEL)

IR - RT BRAKE EXTREMELY WEAK. NR 3 BRAKE AT FAULT, TURNED OFF ANTI-SKID BRAKES, OPS NORMAL. REPLACED NR 3 TRANSDUCEDR ANTI-SKID, OPS NORMAL.

Part: HINGE COVER — CRACKED (RT NLG WW)

FOUND ON D1 LETTER CK - RT NLG WW DOOR HINGE COVER CRACKED IN UPPER RADIUS. REPAIRED PER SRM 51-40-2.

Part: RETRACT MECH — MALFUNCTIONED (LDG GEAR DOORS)

CVG - DURING CLIMBOUT ABOVE 350 KTS AT 17,000 FT, LANDING GEAR DOOR MASTER AND ALL GEAR RED INDICATORS WERE MOMENTARILY FLASHING, ACCOMPANIED BY BRIEF BUFFECTING OF AIRCRAFT. THE ACFT RETURNED TO CVG. JACKED A/C AND RAN GEAR, ALL NORMAL. TIGHTENED AIR GROUND SENSE ARM, RETURNED TO SERVICE.

Part: TRUNNION FITTING — CORROSION (LT/RT MLG)

LIGHT FRETTING CORROSION ON BORES/CAPS AND FACES OF THE LT/RT TRUNNION FITTINGS. LIGHT CORROSION ON LWD BORE OF LT TRUNNION AFT CAP ATTACH BOLT HOLE. REPAIR PER M/M 53-40-0 FIG 811. FOUND A AT HMV.

Part: CLIP — CORRODED (BS 1166)

FOUND DURING CV-2 VISIT, CORROSION ON FORMER STA 1166 AFT SIDE BETWEEN STRINGERS 29L AND 27L. REPLACED SKIN CLIP.

Part: SEAT TRACK — CORRODED (FS 344-380)

FOUND ON CV2 CHECK, REF NR 42 CORROSION ON SEAT TRACK RBL 56 FROM FS 344 TO 380. REPAIRED PER SRM 53-10-5.

Part: SEAT TRACK — CORRODED (FS 344-380)

FOUND ON CV2 CHECK, CORROSION ON SEAT TRACK RBL 56 FROM STA 344 TO 380. REPAIRED PER SRM 53-10-5 FIG 9.

Part: SEAT TRACK — CORRODED (FS 380)

FOUND ON CV2 CHECK, CORROSION ON SEAT TRACK LBL 24 AT STA 380. REPAIRED BY REPLACING SEAT TRACK FROM STA 380 TO 400 PER SRM 53-10-5 FIG 7.

Part: ATTACH BRACKET — CRACKED (NR 2 LE FLAP)

FOUND ON CV2 CHECK NR 2 L/E FLAP ACTUATOR ATTACH BRACKET CRACKED. REPAIR: REPAIRED PER M/M 57-20-21.

Part: SEAT TRACK — CORRODED (FS 1070-1090)

FOUND ON CV2 CHECK, CORROSION ON SEAT TRACK AT RBL 45 BETWEEN STA 1070 AND 1090. REPAIRED SEAT TRACK AS PER SRM 53-10-5 FIG 7.

Part: LE SKIN — DAMAGED (NR 3 TE FOREFLAP)

FOUND ON CV2 CHECK DAMAGE TO L/E SKIN OF NR 3 FOREFLAP O/B OF NR 5 FLAPTRACK. REPAIR: REPAIRED PER SRM 57-50-4.

Part: EEL BATTERY — DISCHARGED (CABIN)

DURING LAYOVER, FOUND FORWARD CABIN EMERGENCY EXIT LIGHT INOP. REPLACE RACK AND BATTERY. OPERATION NORMAL.

Part: NOSE COWL — CRACKED (NR 1 ENG)

DURING A ROUTINE SHOP INSPECTION THE OUTER SKIN OF A NOSE COWL WAS FOUND TO HAVE A CRACK BETWEEN 3 RIVET HOLES AT 3 O/C POSITION. INSTALLED FLUSH DOUBLER PER SRM 54-10-3 FIG 3A.

Part: NOSE COWL — CRACKED (NR 1 ENG)

DURING SHOP INSP, NR 1 ENGINE NOSE COWL WAS FOUND WITH A CRACK IN AFT BULKHEAD INNER ANGLE. INSTALLED DOUBLER PER SRM 54-10-3 FIG 3.