N257GL

Part: BRAKE — FROZEN (MLG) · airframe 36,979 hrs · 44,599 cycles

PILOT REPORTED THAT AFTER DE-ICING THE BRAKES FELT VERY INEFFECTIVE, VERY WEEK STOPPING ACTION, EVEN WHEN APPLIED FIRMLY. MX BRAKES FROZE UP, UNFROZE BRAKES BY APPLYING DE-ICE FLUID. OPERATIONS CHECKED GOOD IAW MM 32-40-00.

Part: ACTUATOR — FAULTY (LT MLG) · airframe 35,612 hrs · 43,118 cycles

PILOT REPORTED THAT ON APPROACH TO LANDING WITH LG HANDLE IN THE DOWN POSITION, ONLY NOSE & RT MAIN GEAR GREEN LIGHTS ILLUMINATED. LG RELAY CB TRIPPED, RAN ALL APPROPRIATE CHECKLISTS & LANDING GEAR MANUALLY EXTENDED NORMALLY. MX R & R THE LT MAIN ACTUATOR IAW TC 1900-3230.10, OPERATIONS & LEAK CHECKED GOOD.

Part: SKIN — DEBONDED (BS 290) · airframe 35,458 hrs · 42,950 cycles

DURING A SCHEDULED INSPECTION, FOUND BELLY SKIN BETWEEN STRINGER 15-16L BS 290 CORRODED & DEBONDED. REPAIRED IAW EO 13-1900-53-081.

Part: STRUCTURE — CRACKED (EMERGENCY EXIT) · airframe 35,458 hrs · 42,950 cycles

DURING A SCHEDULED INSPECTION, FOUND EMERGENCY EXIT 4C LOWER AFT CORNER OF BONDED ASSEMBLY, CRACKED APPROXIMATELY 1 5/8 INCHES. REPAIRED IAW EO 13-1900-52-003.

Part: STRINGER — CRACKED (BS 588.1) · airframe 35,458 hrs · 42,950 cycles

DURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE STRINGER 9R AT BULKHEAD BS 588.1, ONE INCH IN LENGTH. REPAIRED IAW EO 13-1900-53-079.

Part: FRAME — CRACKED (BS 107) · airframe 35,458 hrs · 42,950 cycles

DURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE FRAME FLANGE BS 107 STRINGER 8R. THE CRACK RADIATES TO THE END OF THE FRAME & DOWN APPROXIMATELY .3 INCHES FROM THE UPPER FASTENER, .9 INCHES IN LENGTH. REPAIRED IAW EO 13-1900-53-080.

Part: STRINGER — CRACKED (BS 588.1) · airframe 35,458 hrs · 42,950 cycles

DURING A SCHEDULED INSPECTION FOUND TWO CRACKS IN STRINGER 9L AT BULKHEAD BS 588.1 THAT HAVE CONVERGED TO FORM A TRIANGLE SHAPED PIECE, 1.3 INCHES IN LENGTH. REPAIRED IAW EO 13-1900-57-020.

Part: RIB — CRACKED (RT WING) · airframe 35,458 hrs · 42,950 cycles

DURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE RT INBD WING RIB & FLANGE ANGLE. REPAIRED IAW EO 13-1900-57-021.

Part: SPAR — CRACKED (LT WING) · airframe 35,458 hrs · 42,950 cycles

DURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE LT INBD WING INBD RT FLANGE ANGLE AT FS 288.00 & WING SPAR, ONE INCH IN LENGTH. REPAIRED IAW EO 13-1900-57-020.

Part: DOOR — MISINSTALLED (EMERGENCY EXIT) · airframe 34,095 hrs · 41,382 cycles

PILOT REPORTED THAT THE EMERGENCY DOOR AT 6C WAS NOT PROPERLY SEATED. MX REINSTALLED THE EMER DOOR.

Part: CABLE — BROKEN (PAX DOOR) · airframe 34,086 hrs · 41,369 cycles

PILOT REPORTED THAT THE AIRSTAIR DOOR INTERNAL LOCK CABLE IS BROKEN AND THE DOOR WON'T OPEN. OPEN

Part: CABLE — BROKEN (PAX DOOR) · airframe 34,095 hrs · 41,382 cycles

PILOT REPORTED THAT THE AIRSTAIR DOOR INTERNAL LOCK CABLE IS BROKEN AND THE DOOR WON'T OPEN. MX REPLACED THE LOWER FWD AIRSTAIR DOOR ACTUATOR CABLE, OPS CHECKED GOOD.

Part: FRAME — CRACKED (BS 588.1) · airframe 33,898 hrs · 41,147 cycles

DURING A SCHEDULED ROUTINE INSPECTION, FOUND TWO CRACKS AT FS 588.1 STRINGER 9L, 1.25 INCH IN LENGTH. REPAIRED IAW EO 13-1900-53-019. MAJOR REPAIR.

Part: STRINGER — CRACKED (BS 588.1) · airframe 33,898 hrs · 41,147 cycles

DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN A STRINGER AT FS 588.1 AND STRINGER 9R, 1" IN LENGTH. REPAIRED IAW EO 13-1900-53-022. MAJOR REPAIR.

Part: BULKHEAD — DAMAGED (BS 588.1) · airframe 33,898 hrs · 41,147 cycles

DURING A SCHEDULED ROUTINE INSPECTION, FOUND BULKHEAD AT FS 588.1 DAMAGED JUST UNDER STRINGER 8R, PROTRUDING OUT OF A RIVET APPROX .25". REPAIRED IAW EO 13-1900-53-021. MAJOR REPAIR.

Part: SKIN — CRACKED (BS 588.1) · airframe 33,898 hrs · 41,147 cycles

DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK AT FS 588.1 STRINGER 8L, PROTRUDING UPWARD, 1 INCH IN LENGTH. REPAIRED IAW EO 13-1900-53-020. MAJOR REPAIR.

Part: SKIN — DAMAGED (ELEVATOR) · airframe 33,898 hrs · 41,147 cycles

RT ELEVATOR OTBD EDGE & OTBD T/E DAMAGE APPROX 13" X 15.5". T/E ALSO BUCKLED JUST INBD OF OTBD HINGE ATTACH POINT APPROX 4" X 7". REPAIRED IAW TC 1900-2730.00. MAJOR REPAIR.

Part: SPAR CAP — CRACKED (VERTICAL STAB) · airframe 33,330 hrs · 40,563 cycles

DURING A SCHEDULED ROUTINE INSPECTION, FOUND TWO CRACKS ON THE VERTICAL STAB LT FWD SPAR CAP ANGLE TOP TWO RIVETS, 2 INCHES IN LENGTH. MAINTENANCE REPAIRED IAW EO 12-1900-55-056. MAJOR REPAIR.

Part: SPAR CAP — CRACKED (VERTICAL STAB) · airframe 33,330 hrs · 40,463 cycles

DURING A SCHEDULED ROUTINE INSPECTION, FOUND 2 CRACKS ON THE VERTICAL STAB RT FWD SPAR CAP ANGLE TOP TWO RIVETS, 1.25" IN LENGTH. MAINTENANCE REPAIRED IAW EO 12-1900-55-057. MAJOR REPAIR.

Part: PUMP — FAILED (LOW PRESSURE) · airframe 32,393 hrs · 39,338 cycles

LT ENGINE LOW FUEL PRESSURE ANNUNCIATOR ILLUMINATED IN FLIGHT. TURNED ON THE STANDBY PUMP AND THE ANNUNCIATOR WENT OUT. NO FUEL LEAK NOTED ON POST FLIGHT. MX REPLACED THE LT LOW PRESSURE PUMP IAW BMM 73-10-00, OPS CHECKED GOOD.

Part: FRAME — CRACKED (BS 456) · airframe 32,356 hrs · 39,291 cycles

DURING A SCHEDULED ROUTINE INSPECTION, FOUND CRACK ON THE RT SIDEWALL FS 456 AND STRINGER 10R, FRAME AT STRINGER CUTOUT, .2" IN LENGTH. REPAIRED IAW EO 12-1900-53-032. MAJOR REPAIR

Part: FRAME — CRACKED (BS 456) · airframe 32,356 hrs · 39,291 cycles

DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE FRAME AT FS 456 BETWEEN STRINGER 3 & 4L, FWD CARGO DOOR CUTOUT. REPAIRED IAW EO 12-1900-53-031. MAJOR REPAIR

Part: SPAR — CRACKED (HORIZONTAL STAB) · airframe 32,173 hrs · 39,081 cycles

DURING A SCHEDULED ROUTINE INSPECTION, FOUND FOUR CRACKS IN THE HORIZONTAL STAB AFT SPAR WEB, CRACKS RADIATE FROM LIGHTNING HOLE AT 2, 5, 7& 10 O'CLOCK POSITIONS, 1" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-55-013. MAJOR REPAIR.

Part: FRAME — CORRODED (ZONE 100) · airframe 31,491 hrs · 38,289 cycles

DURING A SCHEDULED ROUTINE INSP, FOUND CORROSION ON THE FRAME AT FS 228.25 APPROX 2" INBD OF STRINGER 14R NEXT TO AN EXISTING REPAIR. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-53-002. MATERIALS UTILIZED ARE INCLUDED IN THE EO.

Part: CABLE — TORN (ZONE 700) · airframe 31,392 hrs · 38,177 cycles

SIG EVENT - PILOT REPORTED THAT THE AIR STAIR DOOR ROPE HAS TORN RUBBER SHEATHING. MX REPLACED THE UPPER AFT CABLE IAW BMM 52-10-02, PN: 1440-40GLA.

Part: WIRE — DAMAGED (CABIN LIGHTS) · airframe 30,538 hrs · 37,196 cycles

CABIN LIGHT PARTIAL OPERATION. MAINTENANCE REPAIRED WIRES TO D436 SPLICE TO 4C AND 6C EMERGENCY LIGHTS IAW BMM 33-20-00, OPS CHECKED GOOD.

Part: SKIN — DELAMINATED (RT WINGLET) · airframe 26,713 hrs

MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP MX FOUND EROSION DAMAGE TO THE TOP OF L/E TIP OF THE RT WINGLET, DELAMENATION ON THE INBD SIDE. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-57-003. MATERIALS UTILIZED ARE INCLUDED IN THE EO.

Part: FRAME — CRACKED (BS 303) · airframe 29,414 hrs · 35,894 cycles

MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP, MX FOUND A CRACK IN THE FRAME AT FS 303 IN THE BEND RADIUS, 1.1" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO10-1900-53-064 AND EO 11-1900-53-001. MATERIALS UTILIZED ARE INCLUDED IN THE EO.

Part: ANGLE — CRACKED · airframe 29,414 hrs · 35,894 cycles

MX FOUND A 1.5" CRACK IN THE BEND RADIUS AT THE RT HEAVY ANGLE AT FS 288. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSP EO 10-1900-53-064. MATERIALS UTILIZED ARE INCLUDED IN THE EO.

Part: RELAY — FAILED (MLG) · airframe 27,680 hrs · 33,784 cycles

UPON APPROACH THE PILOTS REPORTED THAT THE LANDING GEAR DID NOT EXTEND AND THE CIRCUIT BREAKER POPPED. THEY THEN PERFORMED A MANUAL EXTENSION. MAINTENANCE INSPECTED THE LANDING GEAR AND FOUND THE HYDRAULIC POWER PACK WOULD NOT SHUT OFF CAUSING THE CIRCUIT BREAKER TO POP. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR RELAY UNDER THE LT AFT NACELLE REF. GMM 9.3.0. MAINTENANCE PERFORMED NUMEROUS EXTENSION & RETRACTION CHECKS. OPERATIONAL CHECKS WERE GOOD.

Part: SKIN — CORRODED (ZONE 100) · airframe 26,787 hrs · 32,656 cycles

DURING ROUTINE SCHEDULED MX CORROSION WAS FOUND ON THE BELLY SKIN BETWEEN STR 15L AND 15R AT FS 243.25. MAINTENANCE REMOVED CORROSION AND REPAIRED THE AFFECTED AREA IAW EO 09-1900-53-0015. RII INSPECTION COMPLIED WITH IAW EO 09-1900-53-0015. INSPECTION SATISFACTORY.

Part: SKIN — CRACKED (ZONE 200) · airframe 26,787 hrs · 32,656 cycles

DURING ROUTINE SCHEDULED MX A CRACK WAS FOUND ON THE SKIN DOME AT FS 150 BETWEEN STR 1 AND 2 R. CRACK APPROX .3 INCH IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA OF THE DOME SKIN AT F.S. 150 IAW EO 09-1900-53-013. RII INSPECTION COMPLIED WITH IAW EO 09-1900-53-013. INSPECTION SATISFACTORY.

Part: STRINGER — CRACKED (ZONE 100) · airframe 26,787 hrs · 32,656 cycles

MAJOR REPAIR - DURING ROUTINE SCHEDULED MAINTENANCE A CRACK 2.9 INCHES WAS FOUND ON THE BELLY SKIN AT F.S. 303.25 2 INCHES INBOARD FROM RIGHT HAND EDGE OF BELLY SKIN PANEL. REPAIRED THE AFFECTED AREA AT F.S. 243.25 AND CUT AND SPLICED THE STRINGER IAW EO 09-1900-53-014. RII INSPECTION COMPLIED WITH I.A.W. E.O. 09-1900-53-014. INSPECTION SATISFACTORY

Part: SKIN — CRACKED (ZONE 100) · airframe 26,787 hrs · 32,656 cycles

MAJOR REPAIR - DURING ROUTINE SCHEDULED MAINTENANCE A CRACK 2.9 INCHES WAS FOUND ON THE BELLY SKIN AT F.S. 303.25 2 INCHES INBOARD FROM RIGHT HAND EDGE OF BELLY SKIN PANEL. MAINTENANCE REPAIRED THE AFFECTED AREA AT F.S. 303.25 I.A.W. E.O. 09-1900-53-012. RII INSPECTION COMPLIED WITH IAW EO 09-1900-53-012. INSPECTION SATISFACTORY.

Part: BULB — BURNED OUT (INSTRUMENT PANEL) · airframe 26,112 hrs · 31,782 cycles

DURING ROUTINE MAINTENANCE AN INSTRUMENT EMERGENCY LIGHT WAS FOUND BURNED OUT. MAINTANENANCE REMOVED AND REPLACED THE BULB. OPERATIONAL CHECK WAS GOOD.

Part: ANNUNCIATOR — FALSE ACTIVATION (PAX DOOR) · airframe 26,083 hrs · 31,745 cycles

CABIN DOOR ANNUNCIATOR ILLUMINATED DURING TAXI OUT AND ONTO RUNWAY. TAKEOFF ABORTED. MAINTENANCE PERFORMED GROUND OPERATIONAL CHECK OF CABIN DOOR ANNUNCITOR. NO DEFECTS NOTED THIS CLEARS DML 34909 ALL PLACARD REMOVED. REF MM 52-70-00.

Part: SKIN — DENTED (LT WING LE) · airframe 25,874 hrs · 31,479 cycles

MAJOR REPAIR - LT OUTBOARD WING LEADING EDGE BIRDSTRIKE REPAIR AT APPROXIMATELY WS 281 TO 301. DENT APPROXIMATELY 5/8TH INCH DEEP. MAINTENANCE REPAIRED THE LT OUTBAORD LEADING EDGE AT WS 281 TO 301 IAW EO 09-UE257-01. SKIN REPAIRED OUT OF PN 118-110047-81. APPROXIMATELY 19.5 .

Part: SQUAT SWITCH — DIRTY (MLG) · airframe 25,719 hrs · 31,261 cycles

FLIGHT 5189 - PILOTS REPORTED THAT AFTER TAKEOFF THE STALL HEAT ANNUNCIATOR ILLUMINATED AND THEY WERE UNABLE TO PRESSURIZE THE AIRCRAFT. MAINTENANCE INSPECTED AND CLEANED THE LEFT HAND SQUAT SWITCH IAW MM 32-60-05. NO DEFECTS WERE NOTED AND THE OPERATIONAL CHECKS WERE GOOD.

Part: SKIN — DENTED (FUSELAGE) · airframe 25,081 hrs · 30,418 cycles

MAJOR REPAIR - DURING ROUTINE DAILY LINE ENVIRONMENT CONDITIONS A TUG COLLIDED WITH THE AIRCRAFT LEAVING FOUR DENTS BELOW THE CARGO DOOR BETWEEN FS 447.0 TO APPROXIMATELY FS 472.7 BETWEEN STRINGER 11L & 12L. MAINTENANCE REPAIRED AFT FUSELAGE SKIN BETWEEN FS 447.0 TO APPROXIMATELY FS 472.7 BETWEEN STRINGER 11L & 12L IAW BEECH 1900D SRM 51-70. REPAIR AREA APPROXIMATELY 21.8 INCH BY 8.3 INCH 2024 T3 ALUMINUM, RIVETS CR3212, CR3213, Z0426 & Z0470AD.

Part: FRAME — CRACKED (BS 177) · airframe 23,513 hrs · 28,345 cycles

FRAME AT FS 177.35 AND STRINGER 9R CRACKED APPROX .500 INCH IN LENGTH. OPEN

Part: FRAME — CRACKED (BS 163) · airframe 23,513 hrs · 28,345 cycles

FRAME AT FS 163.97 AND STR 9R CRACKED APPROX .40 INCH IN LENGTH - RII REQUIRED TC 8.2.1. OPEN

Part: FRAME — CRACKED (BS 177) · airframe 23,513 hrs · 28,345 cycles

FRAME AT FS 177.35 AND STR 9R CRACKED APPROX .500 INCHES IN LENGTH. **SUPPLEMENTAL INFORMATION WILL BE PROVIDED UPON COMPLETION OF THE REPAIR**

Part: FRAME — CRACKED (BS 163) · airframe 23,513 hrs · 28,345 cycles

FRAME AT FS 163.97 AND STR 9L CRACKED APPROX .40 INCH IN LENGTH. RII REQUIRED TC 8.2.1. MAINT REPAIRED FRAME CRACK AT STRINGER RELIEF HOLE F.S. 163.97 AND STRINGER 9L IAW SRM 51-70. REPAIR APPROX 5 INCHES X 2.7 INCHES. 2024-T3 .071. RII C/W IAW TC 8.2.1

Part: SKIN — CORRODED (BS 213-228) · airframe 23,513 hrs · 28,345 cycles

BELLY SKIN REPAIR DUE TO CORROSION REPAIR. SKIN REPAIR AREA APPROX 31.5 INCHES X 23 INCHES FROM FS 213.25/228.25 AND STRINGERS 13L TO 15R. MAINT REPAIRED BELLY SKIN 15R TO 13L AT/FROM FS 213.25 TO FS 228.25 IAW SRM 51-70. REPAIR DIMENSION 26.250 INCHES X 33.5 INCHES 2024 T3 .025. RII C/W IAW T.C. 8.2.1

Part: SKIN — CORRODED (BS 213-228) · airframe 23,513 hrs · 28,345 cycles

BELLY CORROSION FS 213.25 AND FS 228.25 AT STRINGERS 15R, 16R, 14L/13L AT FS 213.25 AND 15L/14L AT FS 228.25. MAINT REPAIRED DEBONDED STR 15R,15L,14L, FOR FS 213.25 TO FS 228.25 IAW SRM 53-90. STR REPAIR DIMENSIONS APPROX 10.5 INCHES. 2024 T-3. RII C/W IAW TASKCARD 8.2.1.

Part: SKIN — CORRODED (BS 213-228) · airframe 23,513 hrs · 28,345 cycles

BELLY SKIN REPAIR DUE TO CORROSION REPAIR. SKIN REPAIR AREA APPROX 31.5 INCHES X 23 INCHES FROM FS 213.25/228.25 AND STRINGERS 13L TO 15R. OPEN

Part: STRINGER — CRACKED (BS 588 S8-8RL) · airframe 20,910 hrs · 25,124 cycles

STRINGER 8R - 8L CRACKED, CANTED BULKHEAD F.S. 588.10 - REPAIR PENDING

Part: SKIN — CORRODED (BS 223-232) · corrosion level 3 · airframe 20,910 hrs · 25,124 cycles

CORROSION FOUND ON BELLY OF AIRCRAFT FS 223-75 TO 232.75, 3.5 INCHES O/B OF STRINGER 15R TO 4 INCHES LEFT OF STRINGER 16, REPAIR PENDING.

Part: ANGLE — CRACKED (BS 288) · airframe 20,910 hrs · 25,124 cycles

RT HEAVY DOUBLERS CRACKED (ANGLE) AT F.S. 288.0 PN NR 114-430002-7180 (RT)

Part: SPAR — CRACKED (HORIZONTAL STAB) · airframe 20,910 hrs · 25,124 cycles

HORIZONTAL SPAR WEB CRACKED AROUND DEICE TUBE HOLE - REPAIR PENDING.

Part: HINGE — CRACKED (CARGO DOOR) · airframe 20,910 hrs · 25,124 cycles

CARGO DOOR HINGE LUGS CRACKED. REPAIR PENDING EO 05-02.

Part: STRINGER — CRACKED (BS 450 S10R) · airframe 20,910 hrs · 25,124 cycles

STRINGER 10R CRACKED AT F.S. 450.00 - REPAIR PENDING

Part: PAN — CRACKED (EXIT WINDOW) · airframe 17,621 hrs · 21,957 cycles

SEAT 4C, 6C, 6A, EMERG EXIT WINDOWS PAN CRACKED. REMOVED AND REPLACED WINDOW PANS.

Part: DOOR — CORRODED (AIRSTAIR) · airframe 17,001 hrs · 21,278 cycles

AIRSTAIR DOOR HAS CORROSION, REPAIRED.

Part: CONNECTOR — DIRTY (HEADSETS) · airframe 16,524 hrs · 20,763 cycles

NO SIDE TONE IN HEADSETS, CLEANED & ADJUSTED MIC JACKS OPS CK GOOD

Part: MOTOR — MALFUNCTIONED (MLG) · airframe 16,484 hrs · 20,717 cycles

BOTH LOAD METER PEG WHEN GEAR MOTOR CYCLES WITH GEAR UP, PENDING CORRECTIVE ACTION.

Part: GROMMET — FAILED (PRESSURE SEAL) · airframe 14,740 hrs · 18,841 cycles

CABIN PRESSURIZATION SYSTEM FAILED IN FLIGHT, REPLACED PRESSURE SEAL GROMMET AND REINSTALLED OUTFLOW VALVE OPS CHECK GOOD.

Part: TUBE — DISCONNECTED (LT WING) · airframe 14,578 hrs · 18,681 cycles

LEFT BLEED AIR FAIL ANNUC ILLUM. RECONNECTED EVA TUBING ON LEFT WING.

Part: CONTROL PANEL — FAILED (NR 1 DC GEN) · airframe 13,554 hrs · 17,592 cycles

LEFT DC GENERATOR FAILED ON TAKE OFF, REPLACED DC POWER PANEL.

Part: SEALANT · airframe 13,248 hrs · 17,266 cycles

LOUD CRACKLING NOISE IN FLIGHT. DIVERTED A/C TO CYS / REMOVED EXCESSIVE SEALANT FROM FO.'S WINDSHIELD, AS REQUIRED

Part: A/C PACK — MALFUNCTIONED (A/C BAY) · airframe 11,706 hrs · 15,577 cycles

LEFT ENVIRONMENTAL FAIL ON T/O. INSPECTED, COULD NOT DUPLICATE.

Part: METER — FAILED (FUEL FLOW) · airframe 10,680 hrs · 14,336 cycles

LEFT AND RIGHT FUEL FLOW GAUGES FLUCTUATED WHEN POWER ADVANCED, REPLACED FLOW METER

Part: CONTROLLER — INOPERATIVE (ONLY) · airframe 10,686 hrs · 14,344 cycles

CABIN PRESSURIZATION NOT HOLDING, REPLACED CONTROLLER

Part: HANDLE — MALFUNCTIONED (PAX DOOR) · airframe 10,627 hrs · 14,281 cycles

CABIN DOOR ANNUNCIATOR ILLUMINATED ON CLIMB-OUT, INSPECTED RESET CABIN DOOR HANDLE OPS CHECKED GOOD

Part: CONTROL UNIT — MALFUNCTIONED (RUDDER)

UNCOMMANDED RUDDER BOOST IN FLIGHT, PENDING CORRECTIVE ACTION

Part: CONTROL UNIT — MALFUNCTIONED (RUDDER)

UNCOMMANDED RUDDERR BOOST IN FLIGHT, PENDING CORRECTIVE ACTION

Part: ALTIMETER — READS HIGH (COCKPIT)

ENCODER READS 200 FEET HIGH. PROBLEM VERIFIED ON BENCH. (X)