N945UW

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 26,284 hrs · 21,525 cycles

AIRCRAFT NOT GROUNDED: PILOT REPORTS AT 1500' MOVING FLAPS FROM 5 TO FULL FLAP SLAT LEVER DISAGREE ILLUMINATED APPROX. 8 SECONDS THEN FLAP SLAT LOW RATE APPEARED AND STAYED ON UNTIL AFTER LANDING AND SELECTING FLAP LP. MAINTENANCE ACCOMPLISHED SUCCESSFUL BITE TEST IAW FIM 27-53-00-801-802A. OPS TEST GOOD. NO 30 DAY HISTORY.

Part: SKIN — CRACKED (LT WING) · airframe 25,182 hrs · 20,628 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK IN LOWER SKIN ASSEMBLY AT LEFT WING SPAR 2, RIB 10. REPAIRED LOWER SKIN ASSEMBLY PER SRM 57-10-01 REPAIR 54.

Part: LIGHT — TORN (CABIN) · airframe 25,137 hrs · 20,591 cycles

PHL - THE AIRCRAFT WAS NOT GROUNDED. FLOOR ESCAPE LIGHTING STRIP AT 1D TORN. MAINTENANCE REPLD. FLORESCENT LIGHTING STRIP, CHKS OK.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 24,985 hrs · 20,476 cycles

LEFT OVERWING LIGHTS INOPERABLE ON EXTERIOR OF AIRCRAFT. THE AIRCRAFT WAS GROUNDED. MAINTENANCE REPLACED POWER UNIT IAW AMM 33-50-01/400 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,916 hrs · 20,421 cycles

RIGHT FIRST CLASS ISLE EMERGENCY LIGHT WAS INOPERATIVE. REPLACED IAW AMM 33-50-21.

Part: UNKNOWN — ODOR (CABIN) · airframe 22,981 hrs · 18,926 cycles

AFTER TAKEOFF AND CLIMB OUT, A STRONG ODOR PRESENT THRU OUT AIRCRAFT. FLIGHT ATTENDANTS DESCRIBED IT AS A STRONG PLASTIC ODOR. NO SMOKE OBSERVED. THE ODOR DID DISIPATE A LITTLE DURING LEVEL OFF BUT PERSISTED. DECLARED AN EMERGENCY, TURNED OFF BLEEDS AND DUMPED CABIN. ODOR DISIPATED AND PLASTIC ODOR DECREASED SIGNIFICANTLY DURING DESCENT. ON ARRIVAL, VERIFIED RECIRCULATION AND MID EBAY FANS WERE SERVICEABLE. RAN APU, BOTH PACKS, AND ENGINES WITH BLEEDS ON, NO ODORS OR DEFECTS NOTED AT THIS TIME. HIGH POWER ENGINE RUNS PERFORMED IAW EMM 72-00-00-760-118. AIRCRAFT WAS GROUNDED.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 22,473 hrs · 18,490 cycles

COCKPIT EMERGENCY LIGHT WILL NOT ILLUMINATE IN THE ON POSITION. REPLACED FORWARD EMERGENCY LIGHT POWER UNIT. AIRCRAFT WAS GROUNDED.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 22,438 hrs · 18,469 cycles

FOUND THE L1 DOOR SLIDE BUSTLE UNRAVELED. REPLACED EMERGENCY SLIDE.

Part: ACM — FAULTED (LEFT) · airframe 21,691 hrs · 17,905 cycles

AFTER TAKEOFF WITH NR 1 PACK 1 OFF, SMELLED AN ODOR, DID NOT RESET PACK IAW QRH PROCEDURE, OPERATED SINGLE PACK, ODOR DICIPATED. MAINTENANCE PERFORMED A LEFT PACK OPS CHECK AND VISUAL INSPECTION IAW AMM 21-00-00. NO ODOR IN COCKPIT OR CABIN. DURING THE OPS CHECK, THE LEFT PACK FAULTED AND STOPPED RUNNING. COMPLIED WITH FIM TASK 21-51-00-810-802-A. MAINTENANCE REPLACED THE NR 1 ACM IAW AMM 21-51-05.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 21,002 hrs · 17,371 cycles

LOWER EMERGENCY LIGHT EXIT SIGN INOPERATIVE AT RIGHT WING EXIT. RECONNECTED WIRE BAYONET SPLICE (SP6431) BEHIND SIDEWALL PANEL.EXIT MARKER AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW WIRING MANUAL 33-50-50.

Part: SEAL REST — DAMAGED (FUSELAGE) · airframe 20,735 hrs · 17,110 cycles

AIRCRAFT IN BASE MAINTENANCE. DAMAGE ON L1 DOOR CUTOUT, FORWARD SEAL REST AT FR16 BETWEEN STRINGER 5L-6L. REPLACED SEAL REST PER SRM 51-41-01 AND SRM 51-43-01.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 20,735 hrs · 17,110 cycles

AFT RIGHT WING TO BODY FAIRING UPPER EMERGENCY LIGHT LENS CRACKED. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-50-25.

Part: WINDOW — SCRATCHED (ESCAPE HATCH) · airframe 20,735 hrs · 17,110 cycles

AIRCRAFT IN BASE MAINTENANCE. SCRATCHED RIGHT HAND OVERWATER ESCAPE HATCH WINDOW BETWEEN STRINGER 08R-11R. REPLACED ESCAPE HATCH WINDOW PER AMM 56-20-01.

Part: SEAL REST — GOUGED (FUSELAGE) · airframe 20,735 hrs · 17,110 cycles

AIRCRAFT IN BASE MAINTENANCE. GOUGED AFT MAIN CABIN L1 DOOR CUTOUT, LATERAL DOOR SEAL REST. REPLACED DOOR SEAL REST PER SRM 51-41-01, 51-40-02, 51-34-04, 51-34-05 AND 51-34-06.

Part: WINDOW — CRAZED (CABIN) · airframe 20,735 hrs · 17,110 cycles

AIRCRAFT IN BASE MAINTENANCE. LEFT HAND CABIN WINDOW NR 1 CRAZED. REPLACED CABIN WINDOW NR 1 PER AMM 56-20-00.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 20,735 hrs · 17,110 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON UPPER SURFACE COCKPIT FLOOR CROSSBEAM AT FR11 BETWEEN Y90.31 AND Y217.31. REPAIRED COCKPIT FLOOR CROSSBEAM PER EA 263661.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,735 hrs · 17,110 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD CARGO DOOR CUTOUT, DOUBLER BETWEEN FR24 AND FR25. REPLACED DOUBLER PER SRM 51-41-02 AND SRM 51-43-04.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,735 hrs · 17,110 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD CARGO DOOR CUTOUT DOUBLER BETWEEN FR26 AND FR27. REPLACED DOUBLER PER SRM 51-41-02 AND SRM 51-43-04.

Part: SKIN — CHAFED (SERVICE DOOR) · airframe 20,735 hrs · 17,110 cycles

AIRCRAFT IN BASE MAINTENANCE. CHAFED AFT SERVICE DOOR LOWER AFT SIDE INNER SKIN. REPLACED INNER SKIN PER SRM 52-41-02, 51-41-01, 51-43-03 AND 51-46-01.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,735 hrs · 17,110 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD CARGO DOOR CUT OUT, LOWER BEAM BETWEEN FR24 AND FR27. REPLACED BEAM PER SRM 51-43-03 AND SRM 51-43-04.

Part: SKIN — CHAFED (TE FLAP) · airframe 20,735 hrs · 17,110 cycles

AIRCRAFT IN BASE MAINTENANCE. RIGHT HAND WING INBOARD AFT FLAP UPPER SKIN CHAFED BETWEEN RIB 1A-2. REPAIRED AFT FLAP UPPER SKIN PER EA 263550.

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,735 hrs · 17,110 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON MAIN CABIN FORWARD FUSELAGE FLOOR STRUCTURE CROSSBEAM AT FR14 BETWEEN Y304.8R AND Y939.8R. REPAIRED CROSSBEAM PER EA 263639.

Part: SEAL REST — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,735 hrs · 17,110 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD CARGO DOOR CUTOUT FORWARD CORNER SEAL REST. REPLACED SEAL REST PER AARD 53-00-00-3 REPAIR 3 AND AMM 20-10-01.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 20,735 hrs · 17,110 cycles

AIRCRAFT IN BASE MAINTENANCE. GOUGE ON MAIN CABIN RIGHT HAND OUTBOARD SEAT TRACK BETWEEN FR60-FR74 AT STRINGER 15L. REPLACED SEAT TRACK PER SRM 51-43-03, 51-41-01, 51-40-02, 51-40-03 AND 51-40-04.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,735 hrs · 17,110 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON CENTER FUSELAGE RIGHT HAND SEAT TRACK AT FR41 AND +Y276. REPLACED SEAT TRACK PER SRM 51-43-03, 51-43-04 AND 51-41-01.

Part: SUPPORT BRACKET — CORRODED (PAX DOOR) · airframe 20,735 hrs · 17,110 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT PAX DOOR SLIDE MECHANISM FLEXBALL CABLE LOWER SUPPORT BRACKET BETWEEN STRINGER 16R TO STRINGER 17R AT Y27600. REPLACED BRACKET PER SRM 51-42-03, SRM 51-40-02.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 20,735 hrs · 17,110 cycles

AIRCRAFT IN BASE MAINTENANCE. GOUGE ON SEAT TRACK AT FR55 AND Y1340R. REPLACED SEAT TRACK PER PER SRM 51-40-02, SRM 51-43-03, 51-41-01.

Part: HINGE — CORRODED (LT WING) · airframe 20,735 hrs · 17,110 cycles

AIRCRAFT IN BASE MAINTENANCE. RUSTED LEFT REAR SPAR AILERON NR 3 HINGE BEARING AT -Y13751L. REPLACED AILERON NR 3 HINGE PER SRM 57-61-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,735 hrs · 17,110 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON MAIN CABIN FORWARD FUSELAGE FLOOR STRUCTURE, SEAT TRACK UPPER FLANGE BETWEEN FR17 AND Y280R. REPLACED SEAT TRACK PER AARD 53-00-00-3 REPAIR 3, E-190 SRM 51-41-01, SRM 51-41-02, SRM 51-43-03 AND SRM 51-43-04.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,735 hrs · 17,110 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT MAIN CABIN LEFT HAND SEAT TRACK AT -Y280L BETWEEN FR73 AND FR84. REPLACED SEAT TRACK PER SRM 51-40-02, 51-43-01.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,735 hrs · 17,110 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON RIGHT MAIN CABIN FORWARD FLOORBEAM ASSEMBLY UPPER FLANGE BETWEEN FR 17 AND FR 18 AT Y330. REPLACED UPPER FLANGE PER SRM 51-43-02, SRM 51-40-02, AND SRM 51-40-03.

Part: FLOOR SUPPORT — CORRODED (FRAME 19) · corrosion level 2 · airframe 20,735 hrs · 17,110 cycles

CORROSION ON LEFT FORWARD MAIN CABIN FLOOR SUPPORT AT FRAME 19 AND -Y1092. REPLACED FLOOR SUPPORT IAW SRMS 51-40-03, 51-43-02.

Part: SHEAR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,735 hrs · 17,110 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON RIGHT HAND AFT MAIN CABIN FLOOR SHEAR PANEL AT FR 84-85 AT Y1193. REPLACED SHEAR PANEL PER SRM 51-42-01, 51-10-03, 51-12-01, 53-23-10, 51-75-16, 51-42-02, 51-23-04, 51-23-05 AND 51-23-06.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,735 hrs · 17,110 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON LEFT HAND FORWARD MAIN CABIN FLOOR SILL AT FR 15-16 AND -Y1193. REPLACED FLOOR SILL PER SRM 51-43-04, SRM 51-41-02 AND AARD 53-00-00-3 REPAIR 3.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,735 hrs · 17,110 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD PASSENGER DOOR CUTOUT LOWER BEAM BETWEEN FR16 AND FR19 AT -Y1245L. REPLACED LOWER BEAM PER SRM 51-40-02, 51-41-02 AND 51-41-01.

Part: HINGE FITTING — CORRODED (LT WING) · airframe 20,735 hrs · 17,110 cycles

LEFT AILERON, NR 2 HINGE FITTING BEARING RUSTED. REPLACED HINGE FITTING IAW AMM 57-61-01.

Part: UPPER SHEET — CORRODED (FRAMES 85-86) · corrosion level 2 · airframe 20,735 hrs · 17,110 cycles

CORROSION ON LEFT AFT MAIN CABIN UPPER SHEET BETWEEN FRAMES 85-86. REPLACED THE UPPER SHEET IAW 53-00-00-3 REPAIR 3, SRM 51-41-02, AND SRM 51-43-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,735 hrs · 17,110 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON RIGHT AFT MAIN CABIN FLOOR PANEL SUPPORT BETWEEN FR 88 AND FR 90 AT Y939. REPLACED PANEL SUPPORT PER AARD 53-00-00-3 REPAIR 3, SRM 51-42-02, 51-43-01 AND 54-41-01.

Part: SUPPORT FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,735 hrs · 17,110 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON MAIN CABIN FORWARD FUSELAGE FLOOR STRUCTURE SUPPORT FITTING AT FR17 AND Y711.2R. REPLACED SUPPORT FITTING PER SRM 51-43-02.

Part: RIB — CRACKED (VERTICAL STAB) · airframe 20,735 hrs · 17,110 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK ON LEFT HAND SIDE VERTICAL STABILIZER AFT SPAR RIB BETWEEN RIB 9-10. REPLACED RIB PER SRM 51-41-01, 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FRAME 16) · corrosion level 2 · airframe 20,735 hrs · 17,110 cycles

CORROSION ON LEFT MAIN CABIN FLOOR SUPPORT AT FRAME 16 AND -Y1143. REPLACED FLOOR SUPPORT IAW SRM 51-43-02.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-14) · corrosion level 2 · airframe 20,735 hrs · 17,110 cycles

CORROSION ON RIGHT MAIN CABIN FORWARD FUSELAGE FLOOR SUPPORT BETWEEN FRAMES 12 AND 14. REPLACED THE FLOOR SUPPORT IAW SRM 51-41-02 AND 51-43-04.

Part: FLOOR SUPPORT — CORRODED (FRAME 84) · corrosion level 2 · airframe 20,735 hrs · 17,110 cycles

CORROSION ON RIGHT AFT MAIN CABIN FLOOR SUPPORT AT FRAME 84 AND Y1168. REPLACED FLOOR SUPPORT IAW SRM 51-43-04 AND 51-41-02.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,735 hrs · 17,110 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON MAIN CABIN FORWARD FUSELAGE FLOOR SILL BETWEEN FRAME 17 AND FRAME 18. REPLACED SILL IAW SRM 51-43-04, SRM 51-41-02, AARD 53-00-00, REPAIR 3.

Part: GUSSET — CHAFED (SERVICE DOOR) · airframe 20,735 hrs · 17,110 cycles

AIRCRAFT IN BASE MAINTENANCE. CHAFED UPPER FORWARD GUSSET ON AFT SERVICE DOOR UPPER INNER SKIN AREA AT STRINGER 8R AND FR 85. REPLACED GUSSET PER SRM 51-46-01, 51-41-01 AND 51-43-01.

Part: SHEAR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,735 hrs · 17,110 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT MAIN CABIN SHEAR PANEL BETWEEN FRAME 87 AND FRAME 88. REPLACED SHEAR PANEL IAW AARD 53-00-00-3, REPAIR 3.

Part: PANEL — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 20,735 hrs · 17,110 cycles

CORROSION ON LEFT AFT MAIN CABIN SPLICE PANEL BETWEEN FRAMES 87 AND 88 AT -Y1104.9. REPLACED SPLICE PANEL IAW SRM 51-10-03 AND 51-12-01.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,735 hrs · 17,110 cycles

AIRCRAFT IN BASE MAINTENANCE, CORROSION ON FORWARD FUSELAGE COCKPIT FLOOR CHANNEL ASSY AT FRAME 12. REPLACED CHANNEL ASSY IAW SRM 51-10-03 AND 51-41-01.

Part: SHEAR PANEL — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 20,735 hrs · 17,110 cycles

CORROSION ON RIGHT AFT MAIN CABIN FLOOR SHEAR PANEL BETWEEN FRAMES 87 AND 88, BETWEEN +Y548 AND +Y914. REPLACED SHEAR PANEL IAW 53-00-00-3 REPAIR 3 E190 SRM 51-40-01 & SRM 51-42-02.

Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,735 hrs · 17,110 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT MAIN CABIN RIGHT HAND FLOOR SPLICE AT FR90 AND Y660. REPLACED FLOOR SPLICE PER E-DRAWING 170-60001-825.

Part: UPPER SHEET — CORRODED (FRAME 85-86) · corrosion level 2 · airframe 20,735 hrs · 17,110 cycles

CORROSION ON AFT MAIN CABIN SUPPORT PANEL UPPER SHEET BETWEEN FR 85- 86 AT Y279. REPLACED UPPER SHEET IAW SRM 51-40-01, 51-43-03, AND 53-00-00-3.

Part: FLOOR SUPPORT — CRACKED (FRAME 85) · airframe 20,735 hrs · 17,110 cycles

CRACK ON AFT MAIN CABIN FLOOR SUPPORT AT FRAME 85. REPLACED FLOOR SUPPORT IAW SRMS 51-40-02, 51-41-01 & DRAWING 170-65660.

Part: PANEL — CORRODED (FRAMES 84-85) · corrosion level 2 · airframe 20,735 hrs · 17,110 cycles

CORROSION ON AFT MAIN CABIN SUPPORT PANEL BETWEEN FR 84-85. REPAIRED SUPPORT PANEL PER E190 SRM 51-40-02, 51-41-02, AND 51-41-01.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,735 hrs · 17,110 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON RIGHT MAIN CABIN FORWARD FUSELAGE FLOORBEAM AT FR 12 BETWEEN Y355.6 AND Y381. REPLACED FLOORBEAM PER SRM 51-41-02 AND 51-43-01.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,735 hrs · 17,110 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD MAIN CABIN FLOOR DOUBLER BETWEEN -Y457L AND -Y889L AT FR16. REPLACED FLOOR DOUBLER PER AARD 53-00-00-3 REPAIR 3.

Part: CAM — DEFECTIVE (L2 DOOR) · airframe 19,867 hrs · 16,346 cycles

AIRCRAFT WAS GNDED. L2 DOOR VENT FLAP WILL NOT UNLOCK WHEN CLOSING DOOR. REPLACED VENT FLAP CAM PLATE IAW AMM 52-12-25. THIS EVENT IS ASSOCIATED WITH THE EVENT REPORTED ON AALA201604179006.

Part: SUPPORT ARM — DEFECTIVE (L2 DOOR) · airframe 19,867 hrs · 16,346 cycles

AIRCRAFT WAS GNDED. CATERING REPORTED THAT THEY ARE HAVING PROBLEMS UNLOCKING THE GUST LOCK TO 2L DOOR WHEN CLOSING. REPLACED L2 DOOR SUPPORT ARM ASSEMBLY IAW AMM 52-12-30. THIS EVENT IS ASSOCIATED WITH THE EVENT REPORTED ON AALA201604179007.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 19,828 hrs · 16,307 cycles

AIRCRAFT WAS NOT GNDED. AFT FLASHLIGHT NOT HOLDING CHARGE. REPLACED BATTERY PACK IAW AMM 33-51-00 & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: ATTACH FITTING — LACK OF LUBE (ZONE 100) · airframe 19,658 hrs · 16,154 cycles

AIRCRAFT WAS NOT GNDED. R1 DOOR ARMING SLIDE LEVER IS HARD TO ARM. CLEANED & LUBED FLOOR GIRT BAR ATTACH FITTINGS & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: BOTTLE — DISCHARGED (L1 DOOR) · airframe 17,046 hrs · 13,928 cycles

AT GATE AFTER DOORS DISARMED, UPON OPENING L1 DOOR, ASSIST BOTTLE FIRED SLAMMING L1 DOOR OPEN. NO CHUTE DEPLOYMENT. CHARGED ASSIST BOTTLE, LEAK CHECK IS GOOD.

Part: COVER — CRACKED (CABIN) · airframe 16,595 hrs · 13,492 cycles

CE CHECK MAIN CABIN AFT PAX FWD DOOR SURROUND PANEL EXIT LIGHT COVER IS CRACKED & BROKEN. REPLACED AFT PAX FWD DOOR SURROUND PANEL EXIT LIGHT COVER IAW AMM 33-50-19 & OPERATIONS CHECKED IAW JOB CARD 43C2003304.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 16,595 hrs · 13,492 cycles

C3 CHECK MAIN CABIN FLOOR PANEL 241DLF IS DELAMINATED. REPLACED IAW JOB CARD 43C24153013.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 16,595 hrs · 13,492 cycles

C3 CHECK MAIN CABIN FLOOR PANEL 242BRF IS DELAMINATED. REPLACED IAW JOB CARD 43C24153013.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 16,595 hrs · 13,492 cycles

C3 CHECK MAIN CABIN FLOOR PANEL 231ELF IS DELAMINATED. REPLACED IAW TYPICAL REPAIR TR190-5301-13-0782.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 16,595 hrs · 13,492 cycles

C3 CHECK CORROSION ON AFT CARGO DOOR CUT OUT SEAL REST BETWEEN FRAME 78 TO 79, Z-1550, Y593.47. REPLACED SEAL REST IAW SRM 51-42-01.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 16,595 hrs · 13,492 cycles

C3 CHECK CORROSION ON FWD CARGO DOOR CUT OUT LOWER SEAL REST BETWEEN FRAME 25 & 26, Y593.47. REPLACED SEAL REST IAW SRM 51-40-02.

Part: PANEL — CORRODED (FUSELAGE) · airframe 16,595 hrs · 13,492 cycles

C3 CHECK CORROSION ON SHEAR PANEL BETWEEN FRAME 87 TO 88, Z-490 & BETWEEN Y270MM - Y270MM. REPLACED SHEAR PANEL IAW SRM 53-23-10, 51-40-02 & 51-43-01.

Part: BATTERY — DISCHARGED (CABIN) · airframe 16,388 hrs · 13,330 cycles

OVERWING MID EXIT LOCATOR LIGHT & EMER CABIN CEILING PANEL 7 LIGHT INOPERATIVE. R & R NR 3 EMER NICAD BATTERY PACK .

Part: COVER — LOOSE (EVAC SLIDE) · airframe 16,175 hrs · 13,146 cycles

AFT LT SERVICE DOOR SLIDE BUSTLE COVER LOOSE. R & R AFT LT DOOR SLIDE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 15,315 hrs · 12,436 cycles

CENTER CEILING EMERGENCY LIGHT WILL NOT ILLUMINATE AT ROW 13. R & R EMERGENCY NICAD BATTERY.

Part: OIL SYSTEM — OVERSERVICED (APU) · airframe 13,402 hrs · 11,040 cycles

APU PNEUMATICS CAUSING ODOR IN COCKPIT AND CABIN. MAINTENANCE FOUND APU OVERSERVICED. DRAINED OIL TO PROPER LEVEL. RAN PACKS HOT AND COLD 30 MINS. NO ODOR DETECTED,

Part: DOOR — MISALIGNED (CABIN) · airframe 13,129 hrs · 10,817 cycles

MAIN CABIN DOOR WILL NOT SHUT. MAINTENANCE ADJUSTED THE FORWARD PASSENGER DOOR DOWNWARD DISPLACEMENT. OPERATIONAL CHECK IS OKAY.

Part: DOOR — OUT OF ADJUST (CABIN) · airframe 13,125 hrs · 10,812 cycles

FORWARD LEFT ENTRY DOOR (1L) WOULD NOT CLOSE. MAINTENANCE ADJUSTED FORWARD PAX DOOR, CLOSED AND OPENED NUMEROUS TIMES OK FOR CONTINUED SERVICE.

Part: DOOR — OUT OF SEQUENCE (CABIN) · airframe 13,120 hrs · 10,805 cycles

FORWARD LEFT ENTRY DOOR WOULD NOT CLOSE. IT DOES NOT ALIGN WHEN FORCED TO CLOSE. MAINTENANCE LUBED MED MECHANISM AND RESET DOOR SEQUENCE. DOOR OPERATIONAL CHECK IS GOOD.

Part: GLOWSTRIP — BROKEN (CABIN) · airframe 12,986 hrs · 10,721 cycles

FLOOR LIGHT FOR SEATS 5A AND 5C INOPERATIVE. MAINTENANCE REPLACED BROKEN SECTION OF PHOTO LUMINESCENT INDICATOR STRIP LIGHT.

Part: LIGHT — MISSING (CABIN) · airframe 12,981 hrs · 10,717 cycles

STRIP OF FLOOR LIGHTING MISSING AND LOOSE AT ROW 5. MAINTENANCE SECURED LIGHTING STRIP TO FLOOR, CHECKS OK.

Part: STRIP — DETACHED (CABIN) · airframe 12,959 hrs · 10,694 cycles

FLUORESCENT STRIPPING IS DETACHED FROM FLOOR VICINITY OF ROW 5. MAINTENANCE SECURED FLUORESCENT STRIP AT ROW 5.

Part: GLOWSTRIP — DEFECTIVE (CABIN) · airframe 12,322 hrs · 10,260 cycles

FORWARD RIGHT EMERGENCY LIGHT STRIP WITH RED DOTS MISSING. MAINTENANCE INSTALLED NEW PHOTOLUMINESCENT STRIP WITH RED DOTS.

Part: OIL SYSTEM — OVERSERVICED (APU) · airframe 11,922 hrs · 9,936 cycles

FLIGHT 2123, BOS - LGA - COCKPIT AND CABIN HAVE STRONG MUSTY, MOLDY, ACIDIC SMELL. MAINTENANCE FOUND THE APU OVER SERVICED AND REMOVED EXCESS OIL AS REQUIRED. THE APU WAS RUN WITH NO DEFECTS NOTED AT THIS TIME.

Part: STRIKER — STICKS (L2 DOOR) · airframe 10,634 hrs · 8,780 cycles

C2 CHECK - L2 DOOR PNEUMATIC ASSEMBLY DOOR ASSIST STRIKER STICKS. REPLACED L2 DOOR PNEUMATIC ASSEMBLY IAW E190 AMM 52-12-51, PART 2.

Part: RETAINER SEAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,635 hrs · 8,780 cycles

C2 CHECK - LEVEL 2 CORROSION ON FORWARD CARGO DOOR LOWER CUTOUT CENTER SEAL REST BETWEEN FR25 TO FR26, S26R. REPLACED FORWARD CARGO DOOR LOWER CUTOUT CENTER SEAL REST BETWEEN FR25 TO FR26, S26R IAW ERJ-190 SRM 51-41-01/02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,635 hrs · 8,780 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK AT FR84, -Z490, Y273. REPLACED SEAT TRACK AT FR84, -Z490, Y273 IAW EA 201728 AND E190 SRM 53-00-10.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,635 hrs · 8,780 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR12 TO FR20, Z-490, Y273. REPLACED FLOORBEAM BETWEEN FR12 TO FR20, Z-490, Y273 IAW TYPICAL REPAIR # TR190-5300-11-0563.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,635 hrs · 8,780 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOOR SUPPORT ANGLE AT FR86, -Z490, -Y700. REPLACED FLOOR SUPPORT ANGLE AT FR86, -Z490, -Y700 IAW E190 SRM 51-41-01, 51-21-01 AND EMBRAER DRAWING 17065600-445.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,635 hrs · 8,780 cycles

C2 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM AT FR13, Z-490, -Y273. REPLACED FLOORBEAM AT FR13, Z-490, -Y273 IAW TYPICAL REPAIR # TR190-5300-0563, ER-J190 SRM 51-23, 51-40, 51-41 & 51-43.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,635 hrs · 8,780 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOOR WEB BETWEEN FR12 TO FR14, -Z490 & BETWEEN Y1180 TO Y1380. REPLACED FLOOR WEB BETWEEN FR12 TO FR14, -Z490 & BETWEEN Y1180 TO Y1380 IAW TYPICAL REPAIR TR190-5300-11-0563.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,635 hrs · 8,780 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR87, Z-490, Y273. REPLACED FLOORBEAM AT FR87, Z-490, Y273 IAW TYPICAL REPAIR TR190-5300-11-0563.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,635 hrs · 8,780 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR17, Z-490, -Y273. REPLACED FLOORBEAM AT FR17, Z-490, -Y273 IAW TYPICAL REPAIR TR190-5300-11-0563.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,635 hrs · 8,780 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR17, Z-490, Y273. REPLACED FLOORBEAM AT FR17, Z-490, Y273 IAW TYPICAL REPAIR TR190-5300-11-0563.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,635 hrs · 8,780 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SHEAR PLATE BETWEEN FR87 TO FR88, Z-490 & BETWEEN -Y273 TO -Y1060. REPLACED SHEAR PLATE BETWEEN FR87 TO FR88, Z-490 & BETWEEN -Y273 TO -Y1060 IAW EA # 201708 & ER-J190 SRM 51-40-06.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,635 hrs · 8,780 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON UPPER SHEET BETWEEN FR85 TO FR86, -Z490, -Y273. REPLACED UPPER SHEET BETWEEN FR85 TO FR86, -Z490, -Y273 IAW TYPICAL REPAIR 190-5300-11-0563.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,635 hrs · 8,780 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SHEAR PLATE BETWEEN FR87 TO FR88, -Z490, BETWEEN -Y273 TO -Y920. REPLACED SHEAR PLATE BETWEEN FR87 TO FR88, -Z490, BETWEEN -Y273 TO -Y920 IAW TYPICAL REPAIR 190-5300-11-0563 AND E190 SRM 51-40-06.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,635 hrs · 8,780 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SHEAR PLATE BETWEEN FR87 TO FR88, -Z490, BETWEEN -Y273 TO Y273. REPLACED SHEAR PLATE BETWEEN FR87 TO FR88, -Z490, BETWEEN -Y273 TO Y273 IAW TYPICAL REPAIR 190-5300-11-0563 AND E190 SRM 51-40-06.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,635 hrs · 8,780 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON GUSSET PLATE AT FR90, Z-490, Y273. REPLACED GUSSET PLATE AT FR90, Z-490, Y273 IAW EMBRAER DRAWING #170-60001-825.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,635 hrs · 8,780 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK GUSSET AT FR84, -Z490, BETWEEN Y273 TO Y1200. REPLACED SEAT TRACK GUSSET AT FR84, -Z490, BETWEEN Y273 TO Y1200 IAW E190 SRM51-40-06 AND EMBRAER DRAWING 190-65140-801.

Part: MODULE — FAULTY (CABIN) · airframe 10,495 hrs · 8,687 cycles

FLIGHT 2138, LGA- BOS - EMERGENCY LIGHT EICAS MESSAGE AT VARIOUS PHASES OF FLIGHT INCLUDING TOUCHDOWN. EMERGENCY LIGHTS ILLUMINATE IN BOTH COCKPIT AND PAX CABINS. FOLLOWED QRH PROCEDURE BUT DOES NOT RESOLVE THE PROBLEM. MAINTENANCE REMOVED AND REPLACED SPDA NR 1 DISCRETE MODULE AT SLOT NR 11 PER AMM 24-61-05. ALSO REMOVED AND REPLACED FORWARD FLIGHT ATTENDANT PANEL PER AMM 25-25-01. OPERATIONAL CHECKS ARE GOOD, NO FAULTS NOTED ON EICAS.

Part: ROD — BROKEN (NACELLE) · airframe 10,398 hrs · 8,591 cycles

FLIGHT 1465 - PHL-ATL - THE ENGINE PYLON FAIRING DID NOT STOW PROPERLY AFTER TAKEOFF. FLIGHT RETURNED TO PHL AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED BROKEN PYLON FAIRING ATTACH ROD. OPERATIONAL CHECK IS GOOD PER AMM 54-50-23. ALSO REMOVED AND REPLACED FAIRING FORWARD ASSEMBLY PANEL.

Part: POWER UNIT — INOPERATIVE (CABIN) · airframe 10,352 hrs · 8,551 cycles

BOS - EMERGENCY CEILING LIGHT ON ROW 17 INOP. MAINTENANCE REMOVED AND REPLACED RIGHT FORWARD EMERGENCY-LIGHT POWER UNIT PER AMM 33-50-01, OPS CHECK GOOD.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 10,237 hrs · 8,424 cycles

PHOTOLUMINESCENT ESCAPE ROUTE MARKING SYSTEM APPARENTLY 1 FOOT PIECE MISSING ON A/C LEFT. REPLACED PHOTOLUMINESCENT STRIP LIGHT, CHECKS OK.

Part: SEAL — DAMAGED (L1 DOOR) · airframe 10,114 hrs · 8,344 cycles

PHL - 1L DOOR LEAKS AIR IN FLIGHT AND DIFFICULT TO OPEN AND CLOSE ON GROUND - REPORTED BY F/A. REMOVED AND REPLACED DAMAGED LOWER DOOR LINING PANEL SEAL WHICH INTERFERED WITH PROPER DOOR CLOSING. OPS CHECK DOOR OK.

Part: CABLE — INOPERATIVE (CAPTAIN SEAT) · airframe 9,734 hrs · 8,015 cycles

BOS - CAPTAIN'S SEAT LATERAL ADJUSTMENT INOPERATIVE. SEAT MOVES SIDE TO SIDE IN ALL POSITIONS. MAINTENANCE REMOVED AND REPLACED THE CAPTAIN'S SEAT LATERAL CABLE. OPERATIONAL CHECK IS GOOD PER AMM 25-11-01-08.

Part: BOTTLE — LOW PRESSURE (PAX DOOR)

BOS - PASSENGER DOOR 2R ASSIST BOTTLE PRESSURE IS BELOW MINIMUM PRESSURE. MAINTENANCE SERVICED THE 2R DOOR ASSIST BOTTLE TO PROPER PRESSURE PER AMM 52-11-51-03 AND 52-12-51-03.

Part: BOTTLE — LOW PRESSURE (PAX DOOR)

BOS - PASSENGER DOOR 1R ASSIST BOTTLE PRESSURE IS BELOW MINIMUM PRESSURE. MAINTENANCE SERVICED THE 1R DOOR ASSIST BOTTLE TO PROPER PRESSURE PER AMM 52-11-51-03 AND 52-12-51-03.

Part: FLAP SYSTEM — MALFUNCTIONED (WING)

FLIGHT 880, PHL-BOS - ON FINAL APPROACH INTO BOS, THE CREW COULD NOT GET THE FLAP EXTENDED AT POSITION 3 ON ACTUATION. DURING THE GO AROUND AND FOLLOWING QRH PROCEDURES, A SECOND ATTEMPT TO EXTEND THE FLAPS RESULTED IN A FLAP FAIL AT POSITION 2. ON THE THIRD ATTEMPT ALL FLAPS OPERATED CORRECTLY AND THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ACCOMPLISHED FIM TASK 27-51-00-810-802A, FAILURE OF FLAP MOVEMENT, FAULT PROCEDURES 1, 1, AND 11 TRANSITORY CONDITION OF THE FLAP CONTROL SYSTEM. NO SIXTY DAY HISTORY, AC OKAY FOR SERVICE.

Part: SLAT — DAMAGED (LT WING)

FLIGHT 1161, PHL-CLT - DURING CLIMB FLEW THROUGH A FLOCK OF 12 GEESE AND ONE STRUCK THE WING. THE CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. THE FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE ACCOMPLISHED A BIRD STRIKE INSPECTION AND DAMAGE TO LEFT NR 2 AND NR 3 SLAT FOUND TO BE OUT OF LIMITS. A TEMPORARY REPAIR WAS ACCOMPLISHED PER EA 114532. THE FINAL REPAIR TO BE ACCOMPLISHED NO LATER THAN 600 FLC.

Part: ACCUMULATOR — LOW PRESSURE (L2 DOOR)

ATL - L2 DOOR PNEUMATIC EMERGENCY ACCUMULATOR HAS LOW PRESSURE. MAINTENANCE SERVICED THE L2 DOOR EMERGENCY ACCUMULATOR PER M/M 52-12-51-614-801A.

Part: SLIDE — FAILED (L2 DOOR) · airframe 5,613 hrs · 4,487 cycles

PIT - C1 - EES - L-2 DOOR EVACUATION SLIDE FAILED SCHEDULED SLIDE DEPLOYMENT FUNCTIONAL TEST IAW US AIRWAYS JOB CARD 43T20025001. REPLACED SLIDE.

Part: WIRE — DAMAGED (CABIN)

PHL - BOTH LEFT AND RIGHT OVERWING EMERGENCY LIGHTS ON LOWER SIDE WALL INOPERATIVE. MAINTENANCE REPAIRED WIRING. OPERATIONAL CHECK IS SATISFACTORY.

Part: SLIDE — DAMAGED (L1 DOOR)

PHL - WHILE AT THE GATE THE L1 EMERGENCY SLIDE FELL OFF BUSTLE AND RESTED ON THE JETWAY DUE TO STITCHING ON THE SLIDE THAT GAVE WAY. MAINTENANCE REMOVED AND REPLACED THE SLIDE. (S)

Part: FASTENER — MISSING (PAX DOOR)

CLT - UNABLE TO OPEN CABIN DOOR. MAINTENANCE FOUND THE PIN FOR DOOR HANDLE MISSING CIRCLIP. THE PIN HAD MOVED FORWARD AND WAS HITTING THE DOOR STRUCTURE PREVENTING THE DOOR HANDLE FROM OPERATING. THE PIN WAS PUT BACK IN ITS PLACE, REPLACED THE WASHER AND CIRCLIP. THE DOOR OPENS AND SHUTS NORMALLY. (S)

Part: SEAL — UNKNOWN (NLG STRUT) · airframe 1,204 hrs · 994 cycles

FLIGHT 1812, PHL - BOS, CREW STATES, ALTER GEAR RETRACTION EICAS MESSAGE -LG WOW SYS FAIL-. MESSAGE DISAPPEARED AFTER GEAR EXTENSION. RETURNED TO PHL. MAINTENANCE REPACKED THE NOSE STRUT.

Part: MODULE — FAILED (EXTERNAL POWER) · airframe 927 hrs · 776 cycles

FLIGHT 1906, PHL-BDL: AS FLIGHT TAXIED IN TO THE GATE, THE CREW STARTED THE APU. SMOKE BEGAN TO FILL THE CABIN AS PASSENGERS WERE LEAVING THE AIRCRAFT. UPDATED 8/3/07: PILOT REPORT INDICATES THAT WHEN CHANGING FROM GROUND POWER TO EXTERNAL POWER, POWER DROPPED OFF LINE, THEN THE CABIN FILLED WITH SMOKE. MAINTENANCE REPLACED THE EXTERNAL POWER MODULE. NO FURTHER FAULTS.