N933DN

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 40,315 hrs · 26,808 cycles

EMERGENCY LIGHTS ABOVE BOTH AFT OVERWING EXIT DOORS INOPERATIVE. R & R THE B5-230 BATTERY PACK. OPS GOOD.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 40,315 hrs · 26,808 cycles

ROW 25 AB & CD EMERGENCY EXIT SIDEWALL LIGHTS INOPERATIVE. FOUND CONNECTOR P1-2306 NOT FULLY SEATED. CONNECTED THE CONNECTOR AND OP CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 40,315 hrs · 26,808 cycles

FOUND ROW 26 AB+CD EMERGENCY EXIT SIDE WALL LIGHTS INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK ASSY.

Part: UNKNOWN — HAZE (AFT CABIN) · airframe 38,502 hrs · 25,758 cycles

DURING LANDING ROLLOUT, FLIGHT ATTENDANT AT 2L JUMP SEAT REPORTED ODORLESS HAZY IN THE AFT SECTION OF CABIN. MEDIUM AUTO BRAKES ON WITH 1.3 REVERSE DURING LANDING. HAZE DISSIPATED DURING TAXI IN. TROUBLESHOT. PERFORMED HIGH PRESSURE BURNOUT. REPLACE COALESCER BAGS IAW MM. OKAY FOR SERVICE.

Part: FRAME — CRACKED (BS 1437) · airframe 38,298 hrs · 25,651 cycles

AFT ACCESSORY COMPARTMENT, BS 1437 FRAME WEB CRACKED. REMOVED FRAME WEB. REPAIRED IAW ERA 555228-14, REV O.

Part: WEB — CRACKED (FUSELAGE) · airframe 38,298 hrs · 25,651 cycles

AFT ACCESSORY COMPARTMENT, LEFT HAND LOUVER FORWARD WEB ON CANT FRAME 1520 CRACKED. REPAIRED IAW SRM 53-10-03.

Part: DOUBLER — BENT (L1 DOOR) · airframe 38,298 hrs · 25,651 cycles

L1 DOOR FORWARD CORNER, EXTERIOR REPAIR DOUBLER IS BENT. FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 52-10-01. (LP# 2897022)

Part: FRAME — CRACKED (NLG WW) · airframe 38,298 hrs · 25,651 cycles

NOSE GEAR WHEEL WELL RIGHT HAND CUTOUT FORWARD FRAME IS CRACKED AT UPPER CORNER, STA 47. REMOVED AND REPLACED FRAME IAW DWG 9910088.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 38,298 hrs · 25,651 cycles

MAIN CABIN CUSP MEMBRANE BS914 RIGHT HAND SIDE IS CRACKED. CUT OUT DAMAGED SECTION. REPAIRED IAW SRM 53-20-02.

Part: FLANGE — BENT (L1 DOOR) · airframe 37,816 hrs · 25,346 cycles

L1 DOOR FORWARD LOWER EDGE FLANGE BENT. REPAIRED IAW SR 52-01-01 AND 52-00-02.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,378 hrs · 25,108 cycles

OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK B5-229. OPERATION CHECKS GOOD.

Part: CONDUIT — MISROUTED (NLG) · airframe 37,096 hrs · 24,920 cycles

NO NOSE GEAR INDICATION WHEN LANDING. STARTED GO AROUND AND NOSE GEAR INDICATION WENT GREEN. MAINTENANCE FOUND CONDUIT ROUTED INCORRECTLY. REPLACED NOSE GEAR PROXIMITY SENSOR IAW MM. OPS CHECKED OK.

Part: SLIDE — FAILED (TAILCONE) · airframe 36,690 hrs · 24,665 cycles

DURING TAILCONE FUNCTIONAL CHECK, TAIL SLIDE CAME APART. REMOVED AND REPLACED TAILCONE SLIDE.

Part: LANYARD — MISSING (TAILCONE SLIDE) · airframe 35,777 hrs · 24,126 cycles

TAILCONE CORD MISSING ON EMERGENCY HANDLE COVER. INSTALLED CORD. OK FOR SERVICE.

Part: BATTERY PACK — UNSECURE (EMERGENCY LIGHTS) · airframe 33,863 hrs · 22,962 cycles

OVERHEAD EMERGENCY LIGHTS WERE INOPERATIVE FROM ROW 13-21. FOUND BATTERY PACK UNSEATED, SEATED THE BATTERY. OPS CHECKED OK.

Part: LONGERON — CRACKED (BS 1469) · airframe 33,116 hrs · 22,497 cycles

LONGERON 2L CRACKED AT BS 1469. COMPLIED WITH PRI 534906-14, REV O. AND ERA 534906-14, REV O.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 32,494 hrs · 22,131 cycles

L1 DOOR SLIDE PACK CABLE PIN ASSY EXPOSED AND OUT OF SLIDE COVER, NOT SECURING PACK. R & R SLIDE ASSEMBLY IAW AMM.

Part: BULKHEAD WEB — DAMAGED (BS 110) · airframe 31,006 hrs · 21,189 cycles

BS 110, UPPER BULKHEAD WEB DAMAGED. COMPLY WITH ERA 526089-14, REV O.

Part: BULKHEAD WEB — DAMAGED (BS 110) · airframe 31,006 hrs · 21,189 cycles

BS 110, BULKHEAD LOWER WEB DAMAGED. COMPLIED WITH ERA 526088-14, REV O.

Part: LANDING GEAR — COLLAPSED (NOSE) · airframe 31,006 hrs · 21,189 cycles

NOSE GEAR COLLAPSED DURING PUSHBACK. NOSE GEAR R & R IAW NR 92-3220-9-0001.

Part: ANGLE — DAMAGED (BS 110 BULKHEAD) · airframe 31,006 hrs · 21,189 cycles

BS 110, LOWER ANGLE DAMAGED. COMPLY WITH ERA 526227-14.

Part: SUPPORT — DAMAGED (NLG DOOR) · airframe 31,006 hrs · 21,189 cycles

LEFT AND RIGHT NLG AFT STRUT DOOR SUPPORT DAMAGED. R & R DOOR STRUT SUPPORT IAW DWG 5913421.

Part: SKIN — DAMAGED (BS 110-120) · airframe 31,006 hrs · 21,189 cycles

DAMAGE TO FUSELAGE SKIN AT BS 110-120, S28L-S28R. REPAIRED IAW ERA 526084-14, SECTION I.

Part: BRACKET — DAMAGED (NLG ACTUATOR) · airframe 31,006 hrs · 21,189 cycles

NLG RETRACT ACTUATOR BRACKET DAMAGED. R & R NLG RETRACT ACTUATOR BRACKET IAW ERA 526178-14, REV O AND DWG 9911509.

Part: BEAM — DAMAGED (NLG WW) · airframe 31,006 hrs · 21,189 cycles

NLG WHEEL WELL UPPER I-BEAM ASSEMBLY DAMAGED. R & R NLG WHEEL WELL UPPER I-BEAM ASSEMBLY IAW ERA 526178-14, REV O AND DWG 9957865.

Part: SUPPORT — CRACKED (NLG BUNGEE) · airframe 31,006 hrs · 21,189 cycles

BS 110, NLG BUNGEE SUPPORT INSTALLATION CRACKED AND BENT. R & R BUNGEE SUPPORT IAW DWG 9911599.

Part: TRUNNION — DAMAGED (NLG) · airframe 31,006 hrs · 21,189 cycles

RIGHT NLG TRUNNION FITTING DAMAGED. REMOVED, REAMED AND INSTALLED TRUNNION IAW DWG 9910088.

Part: BULKHEAD WEB — DAMAGED (NLG WW) · airframe 31,006 hrs · 21,189 cycles

LEFT SIDE NOSE WHEEL WELL WEB DAMAGED. R & R DAMAGED WEB IAW DWG 9910088.

Part: PANEL — DAMAGED (BS 113) · airframe 31,006 hrs · 21,189 cycles

RELAY SUPPORT PANEL, BS 113, DAMAGED. R & R SUPPORT PANEL AND BRACKETS.

Part: TRUNNION — DAMAGED (NLG) · airframe 31,006 hrs · 21,189 cycles

LEFT NLG TRUNNION DAMAGED. REMOVED, REAMED AND INSTALLED TRUNNION IAW DWG 9910088.

Part: BULKHEAD WEB — DAMAGED (NLG WW) · airframe 31,006 hrs · 21,189 cycles

RIGHT SIDE NOSE WHEEL WEEL WEB DAMAGED. R & R DAMAGED WEB IAW DWG 9910088.

Part: LONGERON — DAMAGED · airframe 31,006 hrs · 21,189 cycles

BS 110, LONGERONS 29L DAMAGED. R & R DAMAGED LONGERON IAW DWG 5911401, SHEET 1, ZONE 12.

Part: SUPPORT — DAMAGED (BS 110) · airframe 31,006 hrs · 21,189 cycles

BS 110, E/E BAY MAIN BATTERY SUPPORTS DAMAGED. R & R DAMAGED SUPPORTS IAW DWG 996454, SHEET 1, ZONE 19 AND 22.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 29,975 hrs · 20,542 cycles

DURING SERVICE CHECK, FOUND OVERHEAD EMERGENCY LIGHTS ROW 35-36 INOPERATIVE. R & R BATTERY PACK IAW AMM. OPERATION CHECKS GOOD.

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 28,528 hrs · 19,606 cycles

DIVERTED DUE TO PRESSURIZATION ISSUES. CABIN ALTITUDE KEPT CLIMBING, CREW HAD TO MANUALLY CLOSE OUTFLOW VALVE, CABIN STILL CONTINUED TO CLIMB. GOT CABIN ALT ON OAP AND WARNING. EMERGENCY DESCENT. MX RAN WIRES FROM CABIN PRESSURE CONTROLLER TO OUTFLOW VALVE MOTORS. REPLACED BOTH CPC'S. REPLACED CABIN PRESSURE CONTROL PANEL IN COCKPIT IAW AMM. PRESSURIZED ACFT, FOUND AFT PRESSURE RELIEF VALVE REMAINS SLIGHTLY OPEN DUE TO DEBRIS. REMOVED DEBRIS AND RESET VALVE. PERFORMED VERIFICATION FLIGHT.

Part: OUTFLOW VALVE — FAILED (CABIN PRESSURE) · airframe 28,525 hrs · 19,604 cycles

LOST AUTO PRESSURIZATION AT FL330 WITH NO CONTROL OF OUTFLOW VALVE. EMERGENCY DECLARED. DESCENDED TO 17K, REGAINED CONTROL OF CABIN ALTITUDE WITH MANUAL CONTROL. NO MASKS DEPLOYED. BOTH CONTROLLERS FAULT OUTFLOW VALVE MOTOR. REPLACED OUTFLOW VALVE ACTUATOR ASSY AND NR 2 AUTO PRESSURE CONTROLLER. NO FAULTS.

Part: LONGERON — CRACKED (BS 1475 L2R) · airframe 28,182 hrs · 19,380 cycles

AFT AIR STAIR AREA UPPER RT SIDE BS 1475 AFT SIDE LONGERON 2R CRACKED. REPAIRED IAW ERA 811699-14 REV O.

Part: ATTACH ANGLE — CRACKED (BS 1520) · airframe 28,182 hrs · 19,380 cycles

EMPENAGE LT SIDE BS 1520 UPPER AFT CORNER OF VENT BOX LOUVERS, VERTICAL ATTACH ANGLE CRACKED. R & R ANGLE IAW SRM 51-31-00 VOL II.

Part: STRINGER CLIP — CRACKED (BS 1488 S2R) · airframe 28,182 hrs · 19,380 cycles

AFT AIR STAIR AREA UPPER RT SIDE BS 1488 LONGERON 2R, STRINGER CLIP CRACKED. R & R STRINGER CLIP IAW SRM 51-30-05 VOL II, PAGE 1, DWG 9464460.

Part: ATTACH ANGLE — CRACKED (BS 1520) · airframe 28,182 hrs · 19,380 cycles

EMPENAGE LT SIDE BS 1520 VENT BOX FORWARD OF INTERIOR UPPER LOUVER VERTICAL ATTACH ANGLE CRACKED. R & R ANGLE IAW SRM 51-30-00, PG 1, VOL II.

Part: HOUSING — CRACKED (BS 1520) · airframe 28,182 hrs · 19,380 cycles

EMPENNAGE RT SIDE, BS 1520 UPPER FORWARD CORNER OF VENT BOX LOUVER HOUSING CRACKED. FABRICATED AND INSTALLED ANGLE IAW PO241277 DWG 5920830 AND SRM 51-30-00, VOL II.

Part: SUPPORT BRACKET — CORRODED (BS 642) · corrosion level 2 · airframe 28,182 hrs · 19,380 cycles

LOWER FUSELAGE UNDERWING BARREL KEELBEAM, DUCT SUPPORT BRACKET CORRODED AT BS 942, RBL 8, MARKED TASK 53-121-23. REMOVED CORRODED BRACKET, INSTALLED NEW BRACKET IAW SRM 51-30-01 VOL II, SRM 51-30-5 VOL II, AMM 20-10-00-001 PAGE I.

Part: CUSP WEB — CORRODED (BS 743) · airframe 28,182 hrs · 19,380 cycles

MAIN CABIN RT STA 743 CUSP WEB UPPER SURFACE CORRODED, TASK 53-211-02. REMOVED RIVETS, BLENDED CORROSION BEYOND LIMITS. ORIG THICKNESS .020, ALLOWABLE .016 REMAINING, .005 MATERIAL LOSS, .015, REMAIN CUSP WEB TO BE REPLACED ON W/O 26709-2400-0048 IAW SRM VOL II 51-30-02, 51-10-03 VOLT I 53-00-01 AND NDT SAM 04-00-06, PAR 4. DELTA SERIAL NR 1672932.

Part: CUSP WEB — CORRODED (BS 722) · airframe 28,182 hrs · 19,380 cycles

DURING CHECK, MAIN CABIN RT BS 722 CUSP WEB UPPER SURFACE CORRODED. R & R CUSP WEB IAW DWG 9911524.

Part: CUSP WEB — CORRODED (BS 702) · airframe 28,182 hrs · 19,380 cycles

MAIN CABIN RT BS 702 CUSP WEB UPPER SURFACE CORRODED. RE-WRITE, TASK 53-211-02, REASON FOR REJECT: CORROSION AT FASTENER WITH CRACK AND 100 PERCENT MATERIAL LOSS. REPLACED CUSP WEB ON WO NR 26709-2400-0004 DELTA SN 1672932.

Part: CUSP WEB — CORRODED (BS 399) · airframe 28,182 hrs · 19,380 cycles

DURING CHECK, MAIN CABIN RT STA 399 CUSP WEB SURFACE CORRODED, INSTALLED NEW WEB FROM BS 390 TO 500 RT IAW DWG 9930538. CORROSION OUT OF LIMITS.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 28,182 hrs · 19,380 cycles

AFT CABIN PRESSURE BULKHEAD DOOR FRAME AREA THRESHOLD, FORWARD AREA HAS CORROSION (CPCP TASK 53-125-02). REMOVED CORROSION FOUND REMAINING MATERIAL WAS OUT OF LIMITS. ERA 511663-14 GENERATED AND COMPLIED WITH.

Part: SUPPORT FITTING — INOPERATIVE · airframe 28,182 hrs · 19,380 cycles

LEFT AND RT RETRACT ACTUATOR SUPPORT FITTINGS INSTALLATION CONFIGURATION DOES NOT MATCH EA 02-093855-03AD. REMOVED SEALANT AROUND NUT OF LT AND RT MLG ACTUATOR SUPPORT FITTINGS OTBD SIDES IN COMPLIANCE WITH EA 02-093855-03AD, STEP 12 AND EA JIC 02-093855-03AD OPN 0201 MEO2 AND EA JIC 02-093855-03AD OPN 0101 MEO1 STEP 15.

Part: CUSP WEB — CRACKED (BS 1364) · airframe 28,182 hrs · 19,380 cycles

CUSB WEB CRACKED, FS 1364. REPAIRED CUSP WEB IAW SRM 53-20-02 VOL 1, LT STA 1364.

Part: CUSP WEB — CRACKED (BS 1395) · airframe 28,182 hrs · 19,380 cycles

RIGHT CABIN CUSP WEB CRACKED, BS 1395. CUT OUT DAMAGED AREA AND INSTALLED REPAIR IAW SRM 53-20-02, FIG 18.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 25,231 hrs · 17,768 cycles

COMPLIED WITH ERA 497351-14 SECTION I REPAIR OF LIGHTNING STRIKE AT LT PAX WINDOW ST 769-788 IAW ERA 497351-14 AN SRM 53-30-03.

Part: SKIN — DAMAGED (CABIN) · airframe 25,231 hrs · 17,768 cycles

TIME LIMITED REPAIR INSTALLED AT LT PAX WINDOW STA 807-826 IAW ERA 497351-14 & SRM 53-30-03 VOL I FIG 4.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 25,231 hrs · 17,768 cycles

DURING PAINT VISIT FOUND LIGHTNING STRIKES ON LEFT WINDOW BELTS AT WINDOWS 29 AND 31. COMPLIED WITH PERMANENT REPAIRS ON WINDOW BELT 29 PER SRM 53-10-03 AND SRM 53-30-03 ON N/R 23454.