N992AT

Part: COVER — UNSECURE (ZONE 200) · airframe 52,938 hrs · 36,961 cycles

TAIL EMG EXIT NEEDS RESECURING. REPLACED AFT EIXT ARMING COVER PER B717 AMM 52-12 (7940018)

Part: OIL SYSTEM — LEAKING (APU) · airframe 52,733 hrs · 36,748 cycles

SMKE - AFTER STARTING APU AND TURNING ON PACKS, CABIN FILLED WITH ACRID, RUBBERY, BURNING VISIBLE SMOKE. TURNED OFF PACKS AND SMOKE DISSIPATED. FOUND APU OIL TANK EMPTY AND BLEED DUCTS CONTAMINATED WITH OIL. CLEANED BLEED DUCTS, REPLACED COALESCER BAGS AND PERFORMED ECS/DUCT BURNOUT WITH ENGINE BLEEDS.(7379712)

Part: SEAL — FOD (ZONE 800) · airframe 52,595 hrs · 36,630 cycles

DIVERTED TO BOS DUE TO R1 GALLEY DOOR HIGH PITCH SQUEAL. CLEANED DEBRIS & LUBED DOOR SEAL, PRESSURIZED AIRCRAFT. NO DEFECTS NOTED.(7584826)

Part: COALESCER BAG — CONTAMINATED (ZONE 100) · airframe 51,965 hrs · 36,043 cycles

SHIP 9535 STARTED APU AND DIRTY, MUSTY SMELL OCCURRED ONCE AIR CAME ON. CALLED MX, UNABLE TO FIX IMEDIATLY. CORRECTIVE ACTION: COALESCER BAGS SOAK IN WATER AND DIRTY CAUSE THE ODOR IN CABIN. FOUND DRAIN LINE CLOGGED AND UNCLOGGED LINE. RAN APU FOR 2 HOURS WITH NO SMELL. (7399952)

Part: SKIN — DAMAGED (ZONE 200) · airframe 50,789 hrs · 35,016 cycles

FUSELAGE DAMAGE AFT OF L1 DOOR. REPAIRED A/C PER ER/A 542469-14 REV A. REF 001-0002:0514-2000 NRC 6 FOR DOCUMENTATION OF WORK PERFORMED. (LP #6956730)

Part: SKIN — GROUND DAMAGE (ZONE 100) · airframe 50,789 hrs · 35,016 cycles

AIRCRAFT SUSTAINED DAMAGE FROM JETWAY CONTACT AT LH FRAME STATION BS 237 BETWEEN STR 18L AND STR 17LH. SUMMARY NRC 001-0002:0514-2001/006 00006: COMPLIED WITH ER/A 542469-14 REV A. ENSURED PRI 542469-14 REV 0 MATCHES FINAL ERA. (LP #0719406)

Part: NONE — NONE (NONE) · airframe 50,789 hrs · 35,016 cycles

DTE TRACKING PER ER/A 542469-14 REV A. REPAIR APPROVAL IS LIMITED TO 12 MONTHS OF SERVICE. ER/A REVISION REQUIRED FOR SERVICE BEYOND THIS LIMIT. DTA REQUIRED IN ACCORDANCE WITH FAA AC 120-93. REPAIR APPROVAL LIMITED TO 12 MONTHS OF SERVICE AFTER ACCOMPLISHMENT OF SECTION II OF ER/A 542469-14 REV A. ENGINEERING AUTHORIZATION (ER/A REVISION) REQUIRED FOR SERVICE BEYOND THIS LIMIT. ASSOCIATED ER/A 14-542469 ADDED FOR AC 9535. **REDEFFERED LOG TO QC, ESTABLISHED MONITOR INSP **. (LP #0718492)

Part: FAIRING — MISSING (COMPRESSOR) · airframe 48,828 hrs · 33,281 cycles

THE #2 ENGINE WAS EXPERIENCING HIGH OIL CONSUMPTION. DURING THE INVESTIGATION, WHEN THE #2 ENGINE COWLS WERE OPENED, MAINTENANCE DISCOVERED THAT THE LOWER LEFT COMPRESSOR FAIRING WAS MISSING. EVIDENCE SHOWS THAT THE FAIRING ATTACHING INSERTS LOOKED TO BE "PULLED OUT" AS EXPECTED WITH A MECHANICAL FAILURE. A FAILURE TO BE INSTALLED WAS RULED OUT. SECONDARY EVIDENCE WAS CORE OIL TUBE DAMAGE (WITH LEAKING) AND A NICK / GOUGE ON THE FUEL TUBE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 48,575 hrs · 33,051 cycles

THE EXTERIOR EMERGENCY ILLUMINATION SYSTEM IS INOPERATIVE. MAINTENANCE FOUND DAMAGE ON PCB OF POWER SUPPLY. THE PCB OF POWER SUPPLY WAS REPLACED PER B717 AMM 33-51. ALSO REPLACED THE EMERGENCY BATTERY AS A PRECAUTION PER B717 AMM 33-51. ALL LIGHT OPERATIONALLY CHECKED GOOD. THE AIRCRAFT IS OK FOR SERVICE. (LP #9376188)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 47,469 hrs · 32,098 cycles

CORROSION TYPE EXFOLATION ON FUSELAGE SKIN (LOWER CUTOUT) AT AFT CARGO COMPARTMENT STA 974. SUMMARY OF NRC 00512: CORROSION LEVEL 2. FUSELAGE SKIN LOWER CUTOUT AT AFT CARGO COMPARTMENT STA 974 WAS REPAIRED PER PRI 610235-14 REV 1 AND ER/A 610235-14 REV ORIGINAL SECTION I PERMANENT REPAIR. ACCOMPLISH ERA 610235-14 REV ORIGINAL SECTION II REPETITIVE INSPECTIONS WITHIN 8,000 FC FROM 32,098 TOTAL FLIGHT CYCLES AS OF 11JUL23 AND REPEAT WITHIN EVERY 8,000 FLIGHT CYCLES THEREAFTER UNDER LOG PAGE 2860677. ASSOCIATED ER/A 14-610235 ADDED FOR AC 9535. (LP #2861337)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 47,568 hrs · 32,186 cycles

ER/A 610235-14; FUSELAGE SKIN AFT CARGO DOOR CUTOUT SKIN AND DOUBLER STA Y=954 TO 994, L-28R IS CORRODED. SUBJECT REPAIR REQUIRES FOLLOW-ON ACTION. ACCOMPLISH ER/A 610235-14, SECTION II REPETITIVE INSPECTION WITHIN 8,000 FLIGHT CYCLES FROM 32,098 TOTAL FLIGHT CYCLES AS OF 11JUL23 AND REPEAT WITHIN EVERY 8,000 FLIGHT CYCLES THEREAFTER. ASSOCIATED ER/A 14-610235 ADDED FOR AC 9535. (LP #2860677)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 47,469 hrs · 32,098 cycles

CORROSION ON FRAME STA Y=1021 LONGERON 30+1.5 IN RH/LH. SUMMARY OF NRC 00513: CORROSION LEVEL 2. FRAME STA Y=1021 LONGERON 30 WAS REPAIRED PER B717 SRM 53-20-07-2R PROCEDURE 3, REPAIR 3. (LP #2857160)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 47,469 hrs · 32,098 cycles

CORROSION ON RH ANGLE CUSP FROM STA Y=200 TO Y=219 AT PAX CABIN. SUMMARY OF NRC 00253: CORROSION LEVEL 2. RH ANGLE CUSP FROM STA Y=160 TO Y=219 WAS REPAIRED PER ERA 609394-14 REV ORIGINAL SECTION I. PERMANENT REPAIR. ASSOCIATED ER/A 14-609394 ADDED FOR AC 9535. (LP #2855905)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 47,469 hrs · 32,098 cycles

CORROSION ON INTERCOSTAL BTW STA Y=946-954 AND LONGERON 30 TO 29RH AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00181: CORROSION LEVEL 2. INTERCOSTAL BTW STA Y=946-954 AND LONGERON 30 TO 29RH AT AFT CARGO COMPARTMENT (C2) WAS REPLACED PER B717 SRM 51-41-02-0G AND 51-41-05-0G. (LP #2848118)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 47,469 hrs · 32,098 cycles

CRACK ON INTERCOSTAL STA 636 X=0 CEILING AREA, FWD CARGO. SUMMARY OF NRC 00507: INTERCOSTAL STA 636 X=0 CEILING AREA WAS REPAIRED PER B717 SRM 51-70-11-2R PROCEDURE 1. (LP #2847519)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 47,469 hrs · 32,098 cycles

CORROSION ON WEB SEVERAL POINTS AT AREA DOOR AFT COMPARTMENT (ENTRY AREA) (C2). SUMMARY OF NRC 00175: CORROSION LEVEL 2. WEB AREA DOOR AFT COMPARTMENT WAS REPLACED PER B717 SRM 51-41-02-0G & 51-41-05-0G. (LP #2846580)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 47,469 hrs · 32,098 cycles

CORROSION ON DOOR JAMB SEVERAL POINTS AT AFT COMPARTMENT (C2). SUMMARY OF NRC 00176: CORROSION LEVEL 2. DOOR JAMB AT AFT COMPARTMENT WAS REPLACED PER B717 SRM 51-41-02-0G & 51-41-05-0G. (LP #2848116)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 47,469 hrs · 32,098 cycles

CORROSION ON FRAME CLIP STA 1002 LONGERON 29RH TO 29LH AT AFT CARGO. SUMMARY OF NRC 00496: CORROSION LEVEL 2. FRAME CLIP STA 1002 LONGERON 29RH TO 29LH WAS REPLACED PER B717 SRM 51-41-02-0G. (LP #2846532)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 47,469 hrs · 32,098 cycles

CORROSION ON RH INBD SEAT TRACK STA Y=215 TO Y=220 AT PAX CABIN. SUMMARY OF NRC 00251: CORROSION LEVEL 2. RH INBD SEAT TRACK STA Y=215 TO Y=220 WAS REPAIRED PER B717 SRM 53-20-52-2R PROCEDURE 5 REPAIR 5. (LP #2843578)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 47,469 hrs · 32,098 cycles

SEAT TRACK ON STA 545 TO STA 560 WAS FOUND CORRODED OUT OF LIMITS PER B717 SRM 53-20-52-1A PROCEDURE 1. SUMMARY OF NRC 00473: CORROSION LEVEL 2. SEAT TRACK ON STA 532 TO 588 WAS REPAIRED PER B717 SRM 53-20-52-2R PROCEDURE 5 REPAIR 5. (LP #2844557)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 47,469 hrs · 32,098 cycles

CORROSION ON FITTING STA 893.5 BELOW FLOOR LEVEL CUSP WEB AREA WAS FOUND. SUMMARY OF NRC 00503: CORROSION LEVEL 2. FITTING SPLICE ON STA 893.5 RH WAS REPLACED PER DWG 9910151 REV CH AND B717 SRM 51-41-05-0G. (LP #2842912)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 47,469 hrs · 32,098 cycles

CORROSION ON FLOOR SUPPORT STA Y=175 BTW X=-20 AND X=-45 AT PAX CABIN W1. SUMMARY OF NRC 00309: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=175 BTW X=-20 AND X=-45 AT PAX CABIN WAS REPLACED PER B717 SRM 51-41-05-0G PAR 8 & 51-41-02-0G PAR 4. (LP #2843312)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 47,469 hrs · 32,098 cycles

EXFOLIATION CORROSION ON DIAPHRAGM STA Y=178 TO Y=198 X=-45 X=-52 AT PAX CABIN W1. SUMMARY OF NRC 00303: CORROSION LEVEL 2. DIAPHRAGM STA Y=178 TO Y=198 X=-45 TO X=-52 WAS REPLACED PER B717 SRM 51-41-02-0G. (LP #2838515)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 47,469 hrs · 32,098 cycles

AFTER CORROSION REMOVAL ON CUSP WEB (LIGHTNING HOLE) STA 539, STA 648, STA 890 TO 907, AND STA 929 TO 935 AREAS WERE FOUD OUT OF LIMITS PER B717 SRM 53-00-55-1A PROCEDURE 1 ALLOWABLE DAMAGE 1 PAR 4 A. SUMMARY OF NRC 00480: CORROSION LEVEL 2. (LIGHTNING HOLE) STA 539, STA 648, AND STA 929 TO 935 WERE REPAIRED PER B717 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4 & (LIGHTNING HOLE) STA 890 TO 907 WAS REPAIRED UNDER NRC 00265. (LP #2838550)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 47,469 hrs · 32,098 cycles

CRACKS ON CUSP WEB STA Y=715 AND Y=897 BELOW SEAT TRACK LBL=44 AT PASSENGER CABIN (CPAX). SUMMARY OF NRC 00265: CUSP WEB STA Y=715 AND Y=897 LBL=44 AT PASSENGER CABIN WERE REPAIRED PER B717 SRM 53-00-55-2R-4 PAR. 5 FIG 221 AND FIG 226. (LP #2837755)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 47,469 hrs · 32,098 cycles

CORROSION ON WIRING CLIPS STA Y=272, Y=291, Y=305, Y=310, Y=539, Y=648, Y=849, Y=875, & Y=885 LBL=57 ALSO Y= 885, Y=886, Y=835, Y=845, Y=848, Y=648, Y=575, Y=737, Y=346, & Y= 309 RBL=57 AT PASSENGER CABIN (CPAX). SUMMARY OF NRC 00266: CORROSION LEVEL 2. WIRING CLIPS STA Y=272, Y=291, Y=305, Y=310, Y=539, Y=648, Y=849, Y=875, & Y=885 LBL=57 ALSO Y=885, Y=886, Y=835, Y=845, Y=848, Y=648, Y=575, Y=737, Y= 346, & Y=309 RBL=57 WERE REPLACED PER B717 SRM 51-41-02-0G. (LP #2837460)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 47,469 hrs · 32,098 cycles

BROKEN FLOOR PANEL 121MF OF FWD CARGO COMPARTMENT (C1). SUMMARY OF NRC 00470: FLOOR PANEL 121MF WAS MANUFACTURED AND REPLACED PER ERA 544901-14 REV A AND INSTALLATION OF FLOOR PANEL 121MF ACCOMPLISHED UNDER TASK CARD 2040-0006. (LP #2837740)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 47,469 hrs · 32,098 cycles

CORROSION ON ANGLE AT L1 DOOR JAM WEB (AFT) STA Y=200 AT PAX CABIN. SUMMARY OF NRC 00438: CORROSION LEVEL 2. ANGLE AT L1 DOOR JAM WEB AFT STA Y=200 AT PAX CABIN WAS REPLACED PER B717 SRM 51-41-05-0G AND 51-41-02-0G. (LP #2835840)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 47,469 hrs · 32,098 cycles

CRACKS ON PAN FWD INNER SIDE PROJECTION BEAMS 1, 3, & 5 AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00372: PAN FWD INNER SIDE PROJECTION BEAMS 1, 3, & 5 AT FWD CARGO COMPARTMENT WERE REPAIRED PER B717-200 SRM 52- 30-02-2R PROCEDURE 1 REPAIR 1. (LP #2836257)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 47,469 hrs · 32,098 cycles

AFTER CORROSION REMOVAL AT THE EDGES OF LIGHTENING HOLE ON CUSP; WEBS AT STA Y=469, Y=508, Y=518, Y=527, Y=546, AND X=58 WERE FOUND OUT LIMITS PER B717 SRM 53-00-00-1A PROCEDURE ALLOWABLE DAMAGE GENERAL PAR. 4.A. SUMMARY OF NRC 00478: CORROSION LEVEL 2. CUSP WEBS AT STA Y=469, Y=508, Y=518, Y=527, Y=546, AND X=58 WERE REPAIRED PER B717 SRM 53-00-55-2R-4. (LP #2834361)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 47,469 hrs · 32,098 cycles

CORROSION WAS FOUND ON ANGLE BTW STA Y=149 TO Y=160 AND RBL 56 AT R1 DOOR CUTOUT AREA. (CPAX). SUMMARY OF NRC 00460: CORROSION LEVEL 2. ANGLE BTW STA Y=149 TO Y=160 AND RBL 56 WAS REPLACE PER DWG 5910085 REV. DJ. ANGLE BTW STA Y=149 TO Y=160 AND RBL 56 AT R1 DOOR CUTOUT AREA. INSTALLATION WILL BE DONE WITH THE NRC 253. (LP #2833058)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 47,469 hrs · 32,098 cycles

AFTER CORROSION REMOVAL, THE EDGES OF LIGHTENING HOLES ON CUSP WEBS AT STA Y=461, Y=488, Y=585, Y=799, TO Y=809; LBL X=58 WERE FOUND OUT LIMITS PER B717 SRM 53-00-00-1A PROCEDURE ALLOWABLE DAMAGE GENERAL PAR. 4.A. SUMMARY OF NRC 00481: CORROSION LEVEL2. CUSP WEBS AT STA Y=461, Y=488, Y=585, Y=799, Y=809; LBL X=58 WERE REPAIRED PER B717 SRM-53-00-55-2R-4. (LP #2834030)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 47,469 hrs · 32,098 cycles

CORROSION REMOVAL ON CUSP WEB STA Y=843 TO Y=846 IS OUT OF LIMITS PER B717 53-00-55-1A PROCEDURE 1 PAR. 4. SUMMARY OF NRC 00492: CORROSION LEVEL 2. CUSP WEB STA Y=843 TO Y=846 WAS REPAIRED PER B717 SRM 53-00-55-2R-4 FIG 215. (LP #2831675)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 47,469 hrs · 32,098 cycles

AFTER CORROSION REMOVAL AT LONGERON 30, STA 965.5 TO 967.5 AND STA 972.5 TO 973.5 WAS FOUND OUT OF LIMITS PER B717 SRM 53-00-00-1A PROCEDURE ALLOWABLE DAMAGE GENERAL PAR. 4.C.(2). SUMMARY OF NRC 00449: CORROSION LEVEL 2. LONGERON 30 BTW STA 965.5 TO 973.5 WAS REPAIRED PER B717 SRM 53-00-05-2R PROCEDURE 3 REPAIR 3. (LP #2832382)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 47,469 hrs · 32,098 cycles

RELATED NRC 261 AFTER CORROSION REMOVAL ON FLOOR SUPPORT STA Y=200 BTW X=6 AND X=-6 FLOOR SUPPORT WAS FOUND OUT OF LIMITS PER B717 SRM 53-00-00-1A ALLOWABLE DAMAGE FIG. 101. SUMMARY OF NRC 00448: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=200 BTW X=6 AND X=-6 WAS REPLACED PER B717 SRM 51-41-02-0G AND 51-41-05-0G. (LP #2831318)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 47,469 hrs · 32,098 cycles

CORROSION ON SEAT TRACK RBL 22 BTW STA 411-413 AT PAX COMPARTMENT. (CPAX). SUMMARY OF NRC 00467: CORROSION LEVEL2. SEAT TRACK RBL 22 BTW STA 411-413 WAS REPAIRED PER B717 SRM 53-20-52-2R PROCEDURE 1 REPAIR 1. (LP #2830244)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 47,469 hrs · 32,098 cycles

AFTER CORROSION REMOVAL ON GALLEY FITTING BTW STA Y=200 AND Y=218 BTW X=-20 WAS FOUND OUT OF LIMITS PER B717 SRM 53-00-00-1A ALLOWABLE DAMAGE FIG. 101 (SHEET 2). SUMMARY OF NRC 0053: CORROSION LEVEL 2. SUPPORT WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #2831431)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 47,469 hrs · 32,098 cycles

EXFOLIATION CORROSION ON FLOOR SUPPORT RH STA Y=198 X=55 LH SIDE AT PAX CABIN. SUMMARY OF NRC 00271: CORROSION LEVEL 2. FLOOR SUPPORT RH STA Y=198 X=55 WAS REPLACED PER B717-200 SRM 51-41-05-0G. (LP #2826207)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 47,469 hrs · 32,098 cycles

CORROSION WAS FOUND AT JAM WEB STA Y=200 ON STRINGER 18. SUMMARY OF NRC 00458: CORROSION LEVEL 2. JAM WEB STA Y=200 ON STRINGER 18 WAS REPAIRED PER B717 SRM 51-70-10-2R PROCEDURE 2 REPAIR 2. (LP #2823464)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 47,469 hrs · 32,098 cycles

CORROSION ON FLOOR SUPPORT STA Y=200 X=10 AT PAX CABIN W1. SUMMARY OF NRC 00275: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=200 X=10 WAS REPLACED PER B717 SRM 51-41-05-0G. (LP #2821504)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 47,469 hrs · 32,098 cycles

CORROSION ON DIAPHRAGM STA Y=198 TO Y=200 BTW X=-30 AND X=-50 (RH SIDE) AT PAX CABIN. SUMMARY OF NRC 00254: CORROSION LEVEL 2. DIAPHRAGM STA Y=198 TO Y=218 BTW X=-30 AND X=-56 (RH SIDE) WAS REPLACED PER DWG 9936534 REV BW. (LP #2821288)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 47,469 hrs · 32,098 cycles

CORROSION ON FLOOR SUPPORT STA Y=175 TO Y=198 X=- 45 AT PAX CABIN W1. SUMMARY OF NRC 00290: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=175 TO Y=198 X=-45 AT PAX CABIN WAS REPLACED PER B717 SRM 51-41-02-0G. (LP #2819821)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 47,469 hrs · 32,098 cycles

CORROSION ON FLOOR SUPPORT L1 ENTRANCE DOOR STA Y=180 AND Y=195 AT PAX CABIN W1. SUMMARY OF NRC 00268: CORROSION LEVEL 2. FLOOR SUPPORT L1 ENTRANCE DOOR STA Y=180 AND Y=195 WAS REPLACED PER B717 SRM 51-41-02-0G AND 51-41-05-0G. (LP #2818795)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 47,469 hrs · 32,098 cycles

CRACK ON ANGLE UPPER BEAM AFTER CORNER AT CABIN PAX L1 DOOR. SUMMARY OF NRC 00128: ANGLE UPPER BEAM AFTER CORNER AT CABIN PAX L1 DOOR WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 7, REPAIR 7. (LP #2819045)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 47,469 hrs · 32,098 cycles

CORROSION ON DIAPHRAGM FROM STA Y=190 TO Y=200 BTW X=50 AND X=57 (L1 DOOR) AT PAX CABIN. SUMMARY OF NRC 00274: CORROSION LEVEL 2. DIAPHRAGM FROM STA Y=190 TO Y=200 BTW X=50 AND X=57 WAS REPAIRED PER B717 SRM 51-70-10-2R REPAIR 2. (LP #2819862)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 47,469 hrs · 32,098 cycles

CRACK CUSP WEB STA Y=218 RBL=54 AT PASSENGER CABIN (CPAX). SUMMARY OF NRC 00272: CUSP WEB STA Y=218 RBL=54 WAS REPAIRED PER B717 SRM 53-00-55-2R REPAIR 4. (LP #2816960)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 47,469 hrs · 32,098 cycles

CRACK ON AFT CARGO DOOR FRAME BTW ANGLE AND LACH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00092: AFT CARGO DOOR FRAME BTW ANGLE AND LACH AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 8 REPAIR 8 FIG 204. (LP #2816372)

Part: WIRE — BURNED (WINDOW DEFOG) · airframe 46,459 hrs · 31,285 cycles

ON A/C WAKE UP ,CB POPPED + ANTI-FOG TURNED ON. C/B LEFT OUT, FOUND FLASH SOOT BY PREVIOUS REPAIR ON CAPT,S SLIDING WINDOW HEAT WIRING MARKED WIP 507047. COLLARED C/B. CAPT CLEARVIEW WINDOW DEFOG WIRE X3 FOUND BURNT + BROKEN AT UPPER AFT CORNER OF WINDOW. B717 WDM 30-42-01 WIP 634799. REPLACED WIRING HARNESS FROM S3-151 TO LEFT CLEAR VIEW WINDOW PER B 717 WDM 30-42-01, OPS TEST GOOD PER B717 AMM 30-42 ,(LP6129746)

Part: FRAME — CRACKED (BS 674) · airframe 46,438 hrs · 31,275 cycles

FRAME CRACKED. STA 674 RH. CONDITION 3. (REF STEP 7). REPLACED FRAME ON AMDS WORK CARD 5310-01436-03B.

Part: HOOK — GOUGED (RT MLG UPLOCK) · airframe 46,438 hrs · 31,275 cycles

RIGHT MLG UPLATCH HOOK FACE GOUGED AT PLUNGER. REMOVED AND REPLACED MAIN LANDING GEAR DOOR LATCH CYLINDER REF B717 AMM 32-34-04 LATCH, ASSY, ML OFF 95-3234-9-0001 41320 ON 95-3234-9-0001 38343. (LP1311898)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 46,062 hrs · 30,999 cycles

LT AND RT LWR AFT EMER LIGHTS INOP. REMOVED AND REPLACED EMER LIGHT BATTERY PACK AT STA. 850R. OPS CHECK GOOD. (LP5743702)

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 45,739 hrs · 30,754 cycles

THE TAIL CONE EMERGENCY WALKWAY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE FOUND THAT THE INTERNAL 5A FUSE IN THE POWER SUPPLY B5-260 HAD BLOWN. THE POWER SUPPLY AND BATTERY PACK WERE REPLACED IAW B717 AMM 33-51-03. ALL OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT IS OK FOR SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 44,611 hrs · 29,989 cycles

THE TAIL COMPARTMENT OVERHEAD AND WALKWAY LIGHTS ARE NOT ILLUMINATING. MAINTENANCE REPLACED THE AFT COMPARTMENT EMERGENCY BATTERY REF AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #5545775)

Part: SCUFF PLATE — CORRODED (FWD CARGO) · airframe 41,755 hrs · 27,972 cycles

FURTHER CORROSION FOUND UPON REMOVAL OF FORWARD CARGO DOOR SCUFF PLATE AROUND FASTENER HOLES - MARKED. NRC 001-0301: 5231-2003/001 00076 REPAIRED PER B717 SRM 53-00-15-2R. (LP #0326750)

Part: UNKNOWN — SMOKE (CABIN) · airframe 41,483 hrs · 27,774 cycles

REPORT OF SMOKE IN THE CABIN ON TAXI IN INTO GATE. DECLARED AN EMERGENCY. MAINTENANCE FOUND EVIDENCE OF OVERHEATED STABILIZER TRIM RELAYS IN THE FWD CARGO WITH ASSOCIATED BURNED WIRING. THE PRIMARY STAB TRIM DRIVE MOTOR, BOTH THE UP & DOWN STABILIZER TRIM RELAYS WERE REPLACED. REPLACED WIRES G9633-21-8, G9633-24-8, G9633-26-8 AND G9633-27-8. ALSO REPAIRED AND RETERMINATED WIRES G9633-22-8 AND G9633-25-8. ALL WIRING IAW WDM 27-41-01. REPLACED FIVE COCKPIT CIRCUIT BREAKERS IAW SWPM 20-60-01. B10-92, B10-93, B10-94, B10-96, AND B10-90. HORIZONTAL STAB PRIMARY TRIM CONTROL SYSTEM CHECKS GOOD IAW AMM 27-41. REPLACED SIX RELAYS IAW WDM 27-43-01. R2-602, R2-603, R2-672, R2-5175, R2-5176 AND R2-5177. COMPLIED WITH RTS TEST OF AUTO-FLIGHT SYSTEMS IAW AMM 22-00. ELECTRONIC INSTRUMENT SYSTEM CHECKED GOOD IAW AMM 31-61. GROUND PROXIMITY WARNING SYSTEM .

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 41,074 hrs · 27,504 cycles

FORWARD PASSENGER CABIN CEILING EMERGENCY LIGHTS WOULD NOT TEST. FOUND BATTERY PACK BAD, B5-227 STA 400R. REPLACED SAME PER AMM 33-51. OPERATIONAL CHECK IS GOOD.

Part: COVER — DAMAGED (EMERGENCY LIGHT) · airframe 40,285 hrs · 26,924 cycles

EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED. R & R THE COVER. OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 40,030 hrs · 26,732 cycles

EMERGENCY LIGHTS AT SEAT ROWS 20B AND 20CD ARE INOPERATIVE. REPLACED THE BATTERY PACK IAW MM 33-51. LIGHTS OPS NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 39,573 hrs · 26,393 cycles

DURING TURN-AROUND CHECK, MAINTENANCE FOUND THAT BOTH OF THE EXTERIOR EMERGENCY FLOOD LIGHTS FOR THE LEFT AND RIGHT WINGS WERE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 39,412 hrs · 26,268 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTING FOR THE TAILCONE WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK FOR THE NOTED LIGHT AND THE OPERATIONAL CHECK WAS GOOD.

Part: SKIN — DELAMINATED (RT SPOILER)

DURING MAINTENANCE CHECK, THE RT OTBD SPOILER WAS FOUND DELAMINATED.

Part: SIGN — INOPERATIVE (CABIN) · airframe 39,046 hrs · 26,010 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGN FOR THE AFT RIGHT OVERWING HATCH WAS INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,862 hrs · 25,852 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT BOTH OF THE MAIN CABIN DOORS EMERGENCY EXIT SIGNS WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND THE OPS CHECKED GOOD.

Part: BATTERY PACK — WEAK (EMERGENCY LIGHTS) · airframe 38,716 hrs · 25,739 cycles

DURING LINE CHECK, MAINTENANCE FOUND TWO EMERGENCY LIGHT BATTERY PACKS WERE WEAK. MAINTENANCE REPLACED THE BATTERY PACKS AND THE OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,052 hrs · 25,216 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING IN THE AFT SECTION OF THE CABIN WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. OPS CHECK WAS GOOD.

Part: COVER — UNSECURE (DOOR SLIDE) · airframe 37,358 hrs · 24,660 cycles

INSPECTION DISCOVERED THAT THE EMERGENCY ESCAPE SLIDE IN THE TAILCONE WAS IMPROPERLY INSTALLED. THE SLIDE COVER WAS NOT SECURED AS DESIGNED. THIS WOULD PREVENT PROPER DEPLOYMENT OF THE ESCAPE SLIDE AND IS NOT IN COMPLIANCE WITH 14 CFR, PART 121.703. THE TAILCONE SLIDE COVER WAS RE-INSTALLED CORRECTLY. NO MENTION OF RII BEING COMPLETED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,077 hrs · 24,436 cycles

AFT FLIGHT ATTENDANTS STATION EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP IAW MM.

Part: HOUSING — CRACKED (EMERGENCY LIGHT) · airframe 37,077 hrs · 24,436 cycles

AFT FLIGHT ATTENDANTS STATION, EMERGENCY LIGHT HOUSING CRACKED. R & R LIGHT HOUSING IAW MM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 35,566 hrs · 23,398 cycles

FORWARD ATTENDANT PANEL, EMER LIGHT SWITCH INOPERATIVE. R & R POWER SUPPLY IAW AMM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 35,566 hrs · 23,398 cycles

OVERWING EMER EVACUATION LIGHT INOPERATIVE. R & R POWER SUPPLY IAW AMM.

Part: SIGN — INOPERATIVE (CABIN) · airframe 35,566 hrs · 23,398 cycles

EXIT SIGN OVER AFT TAIL DOOR INOPERATIVE. R & R SIGN IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 35,566 hrs · 23,398 cycles

EMERGENCY CEILING LIGHT IN FWD SECTION INOPERATIVE. R & R BATTERY PACK IAW AMM.

Part: HOUSING — CRACKED (CABIN) · airframe 35,566 hrs · 23,398 cycles

MID CABIN OVERHEAD CEILING EXIT LIGHT HOUSING CRACKED. R & R LIGHT IAW AMM.

Part: HOUSING — BROKEN (CABIN) · airframe 35,566 hrs · 23,398 cycles

CEILING PANELS NR 4, HAS BROKEN EMER LIGHT BUSHING. R & R EMER LIGHT HOUSING ASSEMBLY IAW MM.

Part: HOUSING — BROKEN (CABIN) · airframe 35,566 hrs · 23,398 cycles

CEILING PANELS NR 13, HAS BROKEN EMER LIGHT BUSHING. R & R EMER LIGHT HOUSING ASSEMBLY IAW MM.

Part: HOUSING — BROKEN (CABIN) · airframe 35,566 hrs · 23,398 cycles

CEILING PANELS NR 9, HAS BROKEN EMER LIGHT BUSHING. R & R EMER LIGHT HOUSING ASSEMBLY IAW MM.

Part: HOUSING — BROKEN (CABIN) · airframe 35,566 hrs · 23,398 cycles

CEILING PANELS NR 5, HAS BROKEN EMER LIGHT BUSHING. R & R EMER LIGHT HOUSING ASSEMBLY IAW MM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 35,566 hrs · 23,398 cycles

ANGLE CRACKED AT BS 1144, LONGERON 2L. R & R ANGLE IAW SRM & DWG.

Part: RIB — CRACKED (RT WING) · airframe 35,566 hrs · 23,398 cycles

RIGHT WING NR 5 SLAT OTBD END SEAL, FOUND THE OTBD END RIB CRACKED AT UPPER FASTENER HOLE. REPAIRED RIB IAW SRM & DWG.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 35,566 hrs · 23,398 cycles

AFT CARGO COMPARTMENT, LT SIDEWALL STRAP SUPPORT CRACKED, BETWEEN BS 1002 - 1022. R & R SUPPORT IAW SRM & DWG.

Part: DUMMY RAIL — CORRODED (FUSELAGE) · airframe 35,566 hrs · 23,398 cycles

FORWARD CABIN AREA, FALSE TRACK CORRODED, BETWEEN BS 160 - 200, RBL 7. R & R FALSE TRACK IAW SRM & DWG.

Part: FLOOR SUPPORT — DELAMINATED (FUSELAGE) · airframe 35,566 hrs · 23,398 cycles

FLIGHT COMPARTMENT ENTRY WAY, FLOOR SUPPORT DELAMINATED AT BS 160, BETWEEN LBL 7 TO RBL 7. R & R SUPPORT IAW SRM & DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 35,566 hrs · 23,398 cycles

L1 DOOR AFT CUT OUT WEB CRACKED AT BS 207, BETWEEN LONGERON 14L - 15L. REPAIRED WEB IAW SRM.

Part: FITTING — CORRODED (R1 DOOR) · airframe 35,566 hrs · 23,398 cycles

R1 DOOR, ESCAPE SLIDE GIRT BAR, AFT FITTING MOUNTING SUPPORT CORRODED. R & R FITTING IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 35,566 hrs · 23,398 cycles

FLOOR SUPPORT CORRODED AT BS 149-5, RBL 44. R & R SUPPORT IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 35,566 hrs · 23,398 cycles

FORWARD CABIN, FLOOR SUPPORT CORRODED AT BS 200, BETWEEN LBL 7 TO RBL 7. R & R SUPPORT IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,566 hrs · 23,398 cycles

SEAT TRACK FWD END CORRODED, BS 200, LBL 22. R & R SEAT TRACK IAW SRM & DWG.

Part: FITTING — CORRODED (R1 DOOR) · airframe 35,566 hrs · 23,398 cycles

R1 DOOR, ESCAPE SLIDE GIRT BAR FWD FITTING MOUNTING SUPPORT CORRODED. R & R FITTING IAW SRM & DWG.

Part: FLOOR PANEL — CORRODED (COCKPIT) · airframe 35,566 hrs · 23,398 cycles

FLIGHT COMPARTMENT, FLOOR PANEL CORRODED BETWEEN CAPTAIN SEAT TRACKS. R & R PANEL IAW SRM & DWG.

Part: PAN — CORRODED (FUSELAGE) · airframe 35,566 hrs · 23,398 cycles

R1 DOOR, LOWER CUT OUT AREA CLOSE OUT PAN CORRODED, BETWEEN BS 160 - 200, RBL 55. R & R PAN IAW SRM & DWG.

Part: DUMMY RAIL — CORRODED (FUSELAGE) · airframe 35,566 hrs · 23,398 cycles

FORWARD CABIN AREA, FALSE TRACK CORRODED, BETWEEN BS 160 - 200, LBL 7. R & R FALSE TRACK IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 35,566 hrs · 23,398 cycles

FORWARD CABIN FLOOR SUPPORT CORRODED AT BS. 200, BETWEEN RBL 7 - 44. R & R SUPPORT IAW SRM & DWG.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 35,566 hrs · 23,398 cycles

MAIN CABIN CUSP WEB CRACKED, BETWEEN BS 655 - 685, RBL 45. REPAIRED CUSP WEB IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 35,566 hrs · 23,398 cycles

MAIN CABIN CUSP WEB CRACKED, BETWEEN BS 655 - 686, LBL 45. REPAIRED CUSP WEB IAW SRM.

Part: LANYARD — DISCONNECTED (EVAC SLIDE) · airframe 36,019 hrs · 23,707 cycles

R1 DOOR EMER EVAC SLIDE LANYARD DISCONNECTED. RECONNECTED LANYARD IAW AMM.

Part: SIGN — DAMAGED (CABIN) · airframe 34,873 hrs · 22,959 cycles

RT OVER GALLEY DOOR EMERGENCY EXIT SIGN LIGHT MISSING LETTERING. INSTALLED SIGN ASSEMBLY IAW AMM.

Part: COVER — LOOSE (L1 DOOR) · airframe 34,243 hrs · 22,565 cycles

L1 DOOR EMERGENCY EVAC SLIDE COVER LOOSE. SECURED COVER ASSEMBLY IAW AMM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 33,867 hrs · 22,302 cycles

FWD FLASHLIGHTS INOPERATIVE. R&R BATTERIES IAW MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 33,867 hrs · 22,302 cycles

AFT FLASHLIGHTS INOPERATIVE. R&R BATTERIES IAW MM.

Part: CHARGER — FAILED (CABIN) · airframe 32,984 hrs · 21,749 cycles

EMERGENCY EXIT LIGHT BATTERY CHARGER FAILED OPERATIONS TEST AT BS 260. R&R CHARGER IAW AMM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 32,984 hrs · 21,749 cycles

MAIN CABIN FLOOR PANEL NR 223 DF DELAMINATED. REPAIRED PANEL IAW SRM.

Part: PANEL — DELAMINATED (CABIN) · airframe 32,984 hrs · 21,749 cycles

MAIN CABIN FLOOR PANEL NR 222 ACF DELAMINATED. REPAIRED PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 32,984 hrs · 21,749 cycles

MAIN CABIN FLOOR PANEL NR 222LF DELAMINATED. R&R PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 32,984 hrs · 21,749 cycles

MAIN CABIN FLOOR PANEL NR 222 ABF DELAMINATED. REPAIRED PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 32,984 hrs · 21,749 cycles

MAIN CABIN FLOOR PANEL NR 222 AVF DELAMINATED. R&R PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 32,984 hrs · 21,749 cycles

MAIN CABIN FLOOR PANEL NR 222 AHF DELAMINATED. REPAIRED PANEL IAW SRM.

Part: INLET — CRACKED (VERTICAL STAB) · airframe 33,871 hrs · 22,310 cycles

VERTICAL STABILIZER RAM AIR INLET CRACKED. REPAIRED STABILIZER ASSEMBLY IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 32,984 hrs · 21,749 cycles

MAIN CABIN FLOOR PANEL NR 222 AGF DELAMINATED. REPAIRED PANEL IAW SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 32,984 hrs · 21,749 cycles

MAIN CABIN FWD OF CENTER TANK-VERTICAL SUPPORT CRACKED AT STATION 665 RBL 20. R&R STIFFENER IAW SRM & DRAWING.

Part: FORMER — CRACKED (FUSELAGE) · airframe 32,989 hrs · 21,758 cycles

FORMER CRACKED AT BS 1022 BETWEEN LONGERON 13L TO LONGERON 14L. R&R FORMER IAW SRM & DRAWING.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 32,984 hrs · 21,749 cycles

AFT CARGO COMPARTMENT FWD BULKHEAD LINER SUPPORTS CRACKED. R&R SUPPORTS IAW SRM.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 32,984 hrs · 21,749 cycles

FWD CARGO DOOR INNER SKIN CRACKED. REPAIRED ANGLE IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 32,984 hrs · 21,749 cycles

LT MAIN CABIN WINDOW FRAME CRACKED AT STATION 908. R&R FRAME IAW MM.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 32,989 hrs · 21,758 cycles

SEAT TRACK SUPPORT FITTING CRACKED AT STATION 737, RBL 44. R&R FITTING IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 32,984 hrs · 21,749 cycles

LT LOUVER UPPER AFT END WEB CRACKED AT FRAME 1200. R&R WEB IAW SRM & DRAWING.

Part: CABLE — LOOSE (TAILCONE) · airframe 32,984 hrs · 21,749 cycles

TAIL CONE EMERGENCY EVAC SLIDE RELEASE CABLE HOLD DOWN TO SLIDE COVER LOOSE. SECURED CABLE IAW AMM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 32,984 hrs · 21,749 cycles

LT LOUVER LOWER ANGLE CRACKED AT FRAME 1189. R&R CLIP IAW SRM & DRAWING.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 32,984 hrs · 21,749 cycles

FLOOR PANELS NR 221WF, 222FF, 222LF, 222RF, 222ABF, 222AHF, 222APF, 222AVF, & 223DF DELAMINATED. REPAIRED PANEL IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 32,989 hrs · 21,758 cycles

SEAT TRACK SUPPORT FITTING CRACKED AT STATION 737, LBL 44. REPAIRED FITTING IAW SRM & DRAWING.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 32,984 hrs · 21,749 cycles

LT MAIN CABIN FLOOR PANELS NR 221UF, 222BF, 222JF, 222PF, 222AAF, 222ACF, 222AGE, 222AMF, & 222ATF DELAMINATED. R&R PANEL IAW AMM & SRM.

Part: PAN — CORRODED (FUSELAGE) · airframe 32,984 hrs · 21,749 cycles

AFT CARGO LOWER DOOR JAMB PAN CORRODED. REPAIRED JAMB IAW SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 32,984 hrs · 21,749 cycles

SHEAR TIE CRACKED AT FORMER 1152 STRINGER 2L. R&R SHEAR TIE IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 32,989 hrs · 21,758 cycles

RT FS FRAME TO WING STRAP CRACKED AT STATION 636. R&R STRAP IAW SRM.

Part: SIGN — UNSECURE (CABIN) · airframe 33,630 hrs · 22,162 cycles

R1 GALLEY EMERGENCY EXIT SIGN FELL OFF. INSTALLED SIGN IAW MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 33,316 hrs · 21,963 cycles

FWD FLASHLIGHT INOP. R & R FLASHLIGHT IAW AMM.

Part: COMPRESSOR — STALLED (NR 2 ENGINE) · airframe 33,008 hrs · 21,770 cycles

INFLIGHT SHUTDOWN/AIR RETURN/DECLARED EMERGENCY. NR 2 ENGINE COMPRESSOR STALL DURING CLIMBOUT. REMOVED AND REPLACED NR 2 ENGINE PER TC.

Part: LENS — MISSING (EXIT SIGN) · airframe 32,328 hrs · 21,364 cycles

EXIT SIGN FORWARD SECTION OF BUSINESS CLASS LENS MISSING. LOCATED AND R-EINSTALLED FORWARD EXIT SIGN PER AMM.

Part: COVER — MISSING (EXIT SIGN) · airframe 31,089 hrs · 20,567 cycles

OVERWING EMERGENCY EXIT SIGN COVER MISSING. INSTALLED COVER PER AMM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 30,654 hrs · 20,256 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER AMM.

Part: LENS — MISSING (CABIN)

RT AFT EMERGENCY EXIT MISSING LOWER EXIT SIGN COVER (OVERWING). INSTALLED RT AFT OVERWING EXIT IDENTIFIER LENS OP CHECK A-OK REF B717AMM 33-51.

Part: STRINGER — CRACKED (FUSELAGE)

AFT FUSELAGE UPPER STRINGER, STA 1146, LONG R2, CRACKED. ACCOMPLISHED UPPER STRINGER REPAIR PER B717 SRM 53-00-05.

Part: DOOR FRAME — CORRODED (FUSELAGE)

FORWARD CARGO DOOR CUTOUT, CORROSION. ACCOMPLISHED SPLICE REPAIR PER B717 SRM 51-32-01 AND 53-20-15.

Part: DOOR FRAME — CRACKED (RT MLG WW)

RIGHT MLG WHEEL WELL DOOR FORWARD CUTOUT FRAME, CRACKED. ACCOMPLISHED FRAME CHANNEL REPAIR PER B717 SRM 53-20-02 AND 51-32-01.

Part: LATCH — CORRODED (FUSELAGE)

FWD AIR STAIRS CONTROL ROD ASSEMBLY CABIN CONTROL LATCH AND BRACKET, CORROSION. ACCOMPLISHED CABIN CONTROL LATCH AND BRACKET REPLACEMENT PER B717 SRM 53-00-00 AND 51-41-01 AND B717 AMM 53-21-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 198, LBL 16 TO LBL 42, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 53-00-00 AND 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 200 TO 256, LBL 15, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 53-00-00 AND 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT TRACK, STA 160 TO 200, LBL 7, CORROSION. ACCOMPLISHED FLOOR SUPPORT TRACK REPLACEMENT PER B717 SRM 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 180, RBL 7 TO RBL 45, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT TRACK, STA 160 TO 200, RBL 7, CORROSION. ACCOMPLISHED FLOOR SUPPORT TRACK REPLACEMENT PER B717 SRM 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 237, BL 0, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 53-00-00 AND 51-41-05.

Part: DOOR FRAME — CRACKED (FUSELAGE)

L1 DOOR FRAME, STA 207, LONG L16, CRACKED. ACCOMPLISHED DOOR FRAME DOUBLER REPAIR PER B717 SRM 51-70-10.

Part: FITTING — CORRODED (FUSELAGE)

FWD GALLEY DOOR FWD AND AFT GIRT BAR FITTING, CORROSION. ACCOMPLISHED FWD AND AFT GIRT BAR FITTING REPLACEMENT PER B717 SRM 53-00-00, 51-10-04 AND 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 200, RBL 7 TO LBL 7, CORROSION. OPEN DEFECT.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 200, RBL 7 TO RBL 45, CORROSION. OPEN DEFECT.

Part: STRINGER — CRACKED (FUSELAGE)

AFT FUSELAGE UPPER STRINGER, STA 1146, LONG L2R, CRACKED. OPEN DEFECT.

Part: SPLICE — CORRODED (FUSELAGE)

AFT CARGO DOOR CUT OUT LOWER JAMB FWD AND AFT SPLICES, CORROSION. ACCOMPLISHED LOWER JAMB FWD AND AFT SPLICES SPLICE REPAIR PER B717 SRM 51-10-04, 53-20-15 AND 51-41-02.

Part: FITTING — CRACKED (RT MLG WW)

RIGHT MLG WHEEL WELL DOOR FORWARD CUT-OUT FRAME O/B SUPPORT ATTACH, CRACKED. OPEN DEFECT.

Part: COVER — MISSING (CABIN)

EXIT LIGHT COVER AT R1 DOOR MISSING. INSTALLED NEW LIGHT COVER AS REQUIRED.

Part: SLIDE — OUT OF POSITION (L1 DOOR)

L1 SLIDE FELL ONTO JET BRIDGE. INSTALLED NEW SLIDE IAW 25-61 AMM AWI REQ & C/W.

Part: GIRT BAR — DIRTY (CABIN)

F/A REPORTS, UNABLE TO ARM THE SLIDE IN THE FLOOR FITTING. CLEANED GIRT BAR, OPS CHECK NORMAL REF M/M 25-60.

Part: BATTERY — DEFECTIVE (CABIN)

EMERGENCY POWER WILL NOT TEST EMERGENCY EXTERNAL LIGHTS WILL NOT SHUT OFF. REMOVED AND REPLACED AFT CARGO BATTERY ASSY. OPS CHECKS NORMAL IAW 717 AMM 33-51. P/N OFF/ON 60-1177-9 S/N OFF 2797 ON 2899.

Part: CYLINDER — LEAKING (RT MLG)

RIGHT HYD QUANTITY LOW LEVEL 2 ALERT ON EAD. TRANSFERRED TO N/R N156442 REPLACE RT MLG RETRACT CYC & UPPER BOLT & REPLACED BOTH RT & LT MLG DOOR BUMPERS SVC HYD TO FULL REF M/M 12-13 & M/M 32-33 & 32-14 OPS & LEAK CHECK GOOD.

Part: PLACARD — MISSING (CABIN)

EXIT PLACARD MISSING IN BUSINESS CLASS. INSTALLED LENS COVER AS REQUIRED.

Part: TIRE — FAILED (LT MLG)

LEFT MAIN TIRE FAILED ON TAKEOFF. REMOVED AND REPLACED MAIN TIRE ASSEMBLY IAW AMM 32-41-01. SERVICED WITH N2 TO CORRECT PRESSURE.

Part: LIGHT — INOPERATIVE (COCKPIT)

BULB IN COCKPIT EMERGENCY LIGHT INOPERATIVE. R&R BULB IN EMERGENCY LIGHT. OPS CHECK GOOD AT THIS TIME.

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY LIGHT IN AFT ACCESSORY IS NOT ILLUMINATED. RELAMPED AFT ACCESSORY EMERGENCY LT ASSY IAW B717 MM 33-51. OPS CHECK.

Part: SKIN — DENTED (FUSELAGE)

FUSELAGE SKIN, STA 200 TO 206, LONG L16L, DENTED. ACCOMPLISHED FUSELAGE SKIN DOUBLER REPAIR PER EA 17-53-01333IR. SEE NR 3615, 3685 AND 4201.

Part: FRAME — DAMAGED (FUSELAGE)

EO 17-5310-2937 AFT LEFT STA 1178 CANTED FRAME INSPECTION IDENTIFIED CONFIGURATION 2 CONDITION 5. ACCOMPLISHED REPAIR TO AFT FUSELAGE FRAME CAP, CANTED STA 1178.225, LEFT SIDE IAW AIRTRAN TASK CARD 17-5310-2980.

Part: FRAME — DAMAGED (FUSELAGE)

EO 17-5310-2895 AFT RIGHT STA 1178 CANTED FRAME INSPECTION IDENTIFIED CONFIGURATION 2 CONDITION 5. ACCOMPLISHED REPAIR TO AFT FUSELAGE FRAME CAP, CANTED STA 1178.225, RIGHT SIDE IAW AIRTRAN TASK CARD 17-5310-2990.

Part: DOOR FRAME — CORRODED (CARGO BAY)

AFT CARGO DOOR JAMB PAN, CORROSION. ACCOMPLISHED CARGO DOOR JAMB PAN SPLICE REPAIR PER B717 SRM 53-20-15 REPAIR 7 FIG 201. SEE NR 3618, 4185 AND 3656.

Part: SKIN — CRACKED (VERTICAL STAB)

VERTICAL STAB RT TIP SKIN CRACKED. REPLACED DAMAGED SKIN IAW EA 17-55-01246IR REFERENCE NRWC N046661. MAJOR REPAIR, FORM 337 SUBMITTED.

Part: DOOR — DAMAGED (MLG)

GEAR DOOR OPEN MESSAGE ON FINAL. PERFORMED OPS CHECK OF LANDING GEAR PER MM 32-30. CHECKS NORMAL.

Part: SKIN — DENTED (FS 218 L17L)

FUSELAGE HAS DENT AT FS 218 LONG 17 LT. REWORKED DENT AND INSTALLED INTERNAL DOUBLER REPAIR 2024T3 .032 PER SRM 53-00-01 REPAIR 2 PG 217.

Part: SKIN — DAMAGED (FUSELAGE)

A/C STRUCK BY CATERING TRUCK UNDERNEATH GALLEY SERVICE DOOR. SKIN FROM BS 171 TO BS203 DAMAGED. INSTALLED FUSELAGE SKIN REPAIR FROM BS 171 TO BS 203 STR 20R TO 23R, MATERIAL USED 2024 T3 .063 - 32 1/2 X 13 1/4, PER B717-SRM 53-00-01 REPAIR 6.

Part: FRAME — DAMAGED (FUSELAGE)

A/C STRUCK BY CATERING TRUCK UNDERNEATH GALLEY SERVICE DOOR. FORMERS AT STA 180 DAMAGED. FABRICATED REPLACEMENT SECTION OF FORMERS STATION 180, MATERIAL 7075 T6 INSTALLED PER B717-SRM 53-00-06 FIG 2.

Part: STRINGER — DAMAGED (FUSELAGE)

A/C STRUCK BY CATERING TRUCK UNDERNEATH GALLEY SERVICE DOOR. STRINGER AND SLICED DAMAGED. INSTALLED REPAIR ON STRINGER SECTION AND SPLICE.

Part: FRAME — DAMAGED (FUSELAGE)

A/C STRUCK BY CATERING TRUCK UNDERNEATH GALLEY SERVICE DOOR. FORMERS AT STA 200 DAMAGED. FABRICATED REPLACEMENT SECTION OF FORMERS STATION 200, MATERIAL 7075 T6 INSTALLED PER B717-SRM 53-00-06 FIG 2.