N906AT

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 51,362 hrs · 36,315 cycles

THE EMERGENCY EXIT SIGNS ARE INOPERATIVE AT STATION 180, STATION 247, AND STATION 706. MAINTENANCE REPLACED THE EMERGENCY BATTERY PACKS B5-235, B5-259, AND B5-120 PER B717 AMM 33-51. OPERATION CHECK WAS NORMAL. (LP #5423934)

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 50,829 hrs · 35,833 cycles

OVERWING DOOR EMERGENCY LIGHTS ARE INOPERATIVE. T/S OVERWING DOOR EMERGENCY LIGHTS PER B717 FIM 33-50-00 810-801. REPLACED THE EMERGENCY LIGHT BATTERY PACK AT LOCATION B5-230 PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. AIRCRAFT OK FOR SERVICE. (LP #6010188)

Part: LATCH — LOOSE (LT MLG DOOR) · airframe 50,658 hrs · 35,670 cycles

SHIP 9582 -GEAR/DE- DURING THE FINAL APPROACH FOR LANDING THE AIRCRAFT INDICATED A "GEAR UNSAFE" CONDITION FOR ALL 3 GEAR POSITIONS. AN EMERGENCY WAS DECLARED WITH ATC, THE QRH WAS COMPLIED WITH, AND THE ALTERNATE GEAR EXTENSION PROCEDURES WERE UTILIZED, WHICH RESULTED IN ALL 3 GOOD DOWN AND LOCKED INDICATIONS. CORRECTIVE ACTION: MAINTENANCE FOUND THE LEFT MAIN LANDING GEAR DOOR LATCH LOOSE AND MISSING TWO NUTS FOR THE ATTACH BOLTS. THE NUTS WERE INSTALLED, AND ALL FOUR NUTS WERE PROPERLY TORQUED. THE LEFT AND RIGHT GEAR DOOR SKIDS WERE REPLACED DUE TO HAVING RUNWAY CONTACT FROM ALTERNATE GEAR EXTENSION. EXCESSIVE AIR WAS REMOVED FROM BOTH THE LEFT AND RIGHT HYDRAULIC SYSTEMS. THE PSEU WAS REPLACED. (LP #6209160)

Part: RELAY — FAULTED (ANTI SKID SYSTEM) · airframe 50,292 hrs · 35,345 cycles

SHIP 9582 -MISC/DE- THE FLIGHT CREW RECEIVED AN "ANTI-SKID FAIL" MESSAGE DURING LANDING GEAR EXTENSION ON APPROACH INTO MSP. AN EMERGENCY WAS DECLARED BY THE CREW. THE MESSAGE EXTINGUISHED BEFORE LANDING. CORRECTIVE ACTION: AFTER LANDING, ALL BRAKE TEMPERATURES WERE NORMAL. MAINTENANCE REPLACED BOTH OF THE LANDING GEAR INTERLOCK RELAYS 1 & 2 (R2-5052 & R2-5037) AND PERFORMED ALL RTS TESTS. THE AIRCRAFT WAS RETURNED TO SERVICE. (LP #5879556)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 49,454 hrs · 34,677 cycles

CORROSION ON INTERNAL SKIN AT STAIRWAY DOOR. SUMMARY OF NRC 00568: CORROSION LEVEL 2. STAIRWAY DOOR ASSEMBLY WAS REPLACED PER B717-200 AMM 52-63-01 420-801. (LP #0104041)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,454 hrs · 34,677 cycles

CRACK PAN ON FWD AND AFT UPPER CORNERS AT (L1) PASSENGER ENTRANCE DOOR INTERNAL STRUCTURE. SUMMARY OF NRC 00176: PAN OF FWD UPPER CORNER AT (L1) PASSENGER ENTRANCE DOOR INTERNAL STRUCTURE WAS REPLACED PER B-717-200 SRM 51-41-02-0G AND 51-41-04-0G PROCEDURE GENERAL AND PAN OF AFT UPPER CORNER WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 3 REPAIR 3. (LP #0095941)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,454 hrs · 34,677 cycles

CRACK ON PASSENGER ENTRANCE DOOR NO.1 BEAM BTW STA Y 160-165 APPROX INTERNAL STRUCTURE (L1). SUMMARY OF NRC 00687: PASSENGER ENTRANCE DOOR NO.1 BEAM BTW STA Y 160-165 APPROX INTERNAL STRUCTURE WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 7 REPAIR 7. (LP #0084432)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 49,454 hrs · 34,677 cycles

CORROSION ON PREVIOUS SPLICE REPAIR ON FRAME STA 974 BTW LONG 30 AND 27 LH IN REF NRC 00216. SUMMARY OF NRC 00685: CORROSION LEVEL 2. PREVIOUS SPLICE REPAIR ON FRAME STA 974 BTW LONG 30 AND 27 LH WERE REPLACED AND INSTALLED PER B717-200 SRM 53-20-07-2R PROCEDURE 3. (LP #0082463)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 49,454 hrs · 34,677 cycles

CORRODED LH TIE TRACK BTW STA Y=902/1022 AT AFT CARGO COMPARTMENT AREA WAS REWORKED AND IS OUT OF LIMITS. SUMMARY OF NRC 00683: CORROSION LEVEL 2. LH TIE TRACK BTW STA Y=902/1022 AT AFT CARGO COMPARTMENT WAS REPLACED AND INSTALLED PER B717 SRM 51-41-01-0G AND 51-41-05-0G. (LP #0080988)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 49,454 hrs · 34,677 cycles

DIMENSIONAL MEASUREMENTS WERE FOUND OUT OF LIMITS ON SECTION OF WING BOX UPPER SKIN BTW STA Y=750 AND X=19 TO X=59 AT LH MLG/ WHEEL WELL (SM) AFTER CORROSION REMOVAL. SUMMARY OF NRC 00640: CORROSION LEVEL 2. DIMENSIONAL MEASUREMENTS WERE FOUND OUT OF LIMITS ON SECTION OF WING BOX UPPER SKIN BTW STA Y=750 AND X=19 TO X=59 AT LH MLG/ WHEEL WELL. UPPER REAR SKIN WAS REPAIRED PER ER/A 613283-14 REV ORIGINAL SECTION I PERMANENT REPAIR AND PRI 613283-14 REV 6. ASSOCIATED ER/A 14-613283 ADDED FOR AC 9582 (LP #0081393)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,454 hrs · 34,677 cycles

CRACKS ON CORNER FWD ON SCUFF PLATE AT AFT CARGO. SUMMARY OF NRC 00002: SCUFF PLATE AT AFT CARGO WAS REPAIRED PER ER/A 542149-14TR REV B. SECTION I, PERMAMENT REPAIR. ASSOCIATED ER/A 14-542149 ADDED FOR AC 9582. (LP #0075763)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 49,454 hrs · 34,677 cycles

CORROSION ON FRAME CLIP STA Y=946 AND BTW LONG 29R/28L AT AFT CARGO COMPARTMENT, WAS FOUND TO BE OUT OF LIMITS. SUMMARY OF NRC 00636: CORROSION LEVEL 2. FRAME CLIP WAS REPLACED PER DWG 9919603 REV CC AND B717 SRM 51-41-02-0G AND 51-41-05-0G. (LP #0074154)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,454 hrs · 34,677 cycles

CRACK ON UPPER AFT CORNER OF FUSSELAGE SKIN AT LH SLIDING WINDOW CUTOUT IN REF TO NRC 00651. SUMMARY OF NRC 00663: UPPER AFT CORNER OF FUSSELAGE SKIN AT LH SLIDING WINDOW CUTOUT WAS REPAIRED PER B717-200 SRM 56-10-02-2R PROCEDURE 1 REPAIR 1. (LP #0069478)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 49,454 hrs · 34,677 cycles

CORROSION ON WEB BTW STA Y=954/994 AND BTW LONG=28R/29R AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00220: CORROSION LEVEL 2. WEB BTW STA Y=954/994 AND BTW LONG=28R/29R AT AFT CARGO COMPARTMENT WAS REPLACED AND INSTALLED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #0065439)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,454 hrs · 34,677 cycles

CRACK ON LONGERON 2RH STA Y=1133 AT AFT ACCESSORY. SUMMARY OF NRC 00660: CRACK ON LONGERON 2RH STA Y=1133 AT AFT ACCESSORY WAS REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2, REPAIR 2. (LP #0063433)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,454 hrs · 34,677 cycles

CRACK ON LONGERON 2RH STA Y=1133 AT AFT ACCESSORY. SUMMARY OF NRC 00660: CRACK ON LONGERON 2RH STA Y=1133 AT AFT ACCESSORY WAS REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2, REPAIR 2. (LP #0063330)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 49,454 hrs · 34,677 cycles

CORROSION ON DOOR JAMB AFT CARGO COMPARTMENT STA Y 960 TO STA Y 986 C2. SUMMARY OF NRC 00040: CORROSION LEVEL 2. DOOR JAMB AFT CARGO COMPARTMENT STA Y 960 TO STA Y 986 C2 WAS REPLACED AND INSTALLED PER B717-200 SRM 53-20-15-2R PROCEDURE 7, 51-41-02-0G, AND 51-41-05-0G. (LP #0058644)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 49,454 hrs · 34,677 cycles

CORROSION ON (Y CHORD) FRAME OF BULKHEAD STA Y=1053 AND BTW LONG 28L/28R AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00229: CORROSION LEVEL 2. (Y CHORD) FRAME OF BULKHEAD STA Y=1053 AND BTW LONG 28L/28R AT AFT CARGO COMPARTMENT WAS REPLACED AND INSTALLED PER B717-200 SRM 51-41-05-0G AND 51-41-02-0G. (LP #0053021)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 49,454 hrs · 34,677 cycles

CORROSION ON AFT PRESSURE BULKHEAD SKIN LOWER AREA STA Y=1053 AND BTW LONGERON 27R/27L AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00428: CORROSION LEVEL 2. AFT PRESSURE BULKHEAD SKIN LOWER AREA STA Y=1053 AND BTW LONGERON 27R/27L AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-08-2R PROCEDURE 7 REPAIR 7. (LP #0049430)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,454 hrs · 34,677 cycles

CRACK ON LOWER SURFACE OF CUSP WEB STA Y 217 TO STA Y237 AND X=56 AT CPAX. SUMMARY OF NRC 00397: CUSP WEB STA Y 217 TO STA Y237 AND X=56 WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4. (LP #0048292)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,454 hrs · 34,677 cycles

CRACK ON CUSP WEB BTW STA 651 TO STA 661 AND X=56 AT CPAX. SUMMARY OF NRC 00374: CUSP WEB BTW STA 651 TO STA 661 AND X=56 AT CPAX WAS REPAIRED PER B717-200 SRM 53-00-55 REPAIR 4. (LP #0048006)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 49,454 hrs · 34,677 cycles

CORROSION ON RH CUSP WEBS BTW ON STA Y=470, Y=493, AND Y=526 X=-56 AT PAX CABIN. SUMMARY OF NRC 00566: CORROSION LEVEL 2. RH CUSP WEBS BTW ON STA Y=470, Y=493, AND Y=526 X=-56 AT PAX CABIN. WERE REPAIRED PER B717 SRM-53-00-55-2R PROCEDURE 4 REPAIR 4 AND SRM 51-41-02-0G. (LP #0045074)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 49,454 hrs · 34,677 cycles

CORROSION ON FLOOR SUPPORTS STA Y 148 TO STA Y 200 AND X=7 AND STA Y 162 TO STA Y 195 AND X=56 AT PASSENGER CABIN. IN REF NRC 0395. W1. SUMMARY OF NRC 00559: CORROSION LEVEL 2. SUPPORTS STA Y 148 TO STA Y 200 AND X=7 AND STA Y 162 TO STA Y 195 AND X=56 WERE REPLACED AND INSTALLED PER DWG 9936534-71 REV BW, B717-200 SRM 51 -41-02-0G, 51-41-05-0G, AND 51-41-01-0G. (LP #0045301)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 49,454 hrs · 34,677 cycles

CORROSION ON FLOOR SUPPORT STA 185 TO 194 X=54 AT PASSENGER CABIN. W1. SUMMARY OF NRC 00521: CORROSION LEVEL 2. FLOOR SUPPORT STA 185 TO 194 X=54 AT PASSENGER CABIN WAS MANUFACTURED AND INSTALLED PER DWG 9936534-101 REV BW AND B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #0044887)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 49,454 hrs · 34,677 cycles

CORROSION ON WEB STA Y 185 TO STA Y 200 BTW X=49 TO X=56 AT CPAX (W1). SUMMARY OF NRC 00396: CORROSION LEVEL 2. WEB STA Y 185 TO STA Y 200 BTW X=49 TO X=56 AT CPAX (W1) WAS REPAIRED PER B717-200 SRM 51-70-10-2R-1 FIG 201. (LP #0043371)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,454 hrs · 34,677 cycles

CORROSION ON RH OUTBD SEAT TRACK REPAIR PLUG BTW STA 984 TO 988 PAX CABIN. SUMMARY OF NRC 00638: CORROSION LEVEL 1. SEAT TRACK REPAIR PLUG WAS REPLACED PER B717-200 SRM-53-20-52-2R PROCEDURE 1 REPAIR 1 AND 51-41-01-0G. (LP #0042043)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 49,454 hrs · 34,677 cycles

CORROSION ON FLOOR SUPPORT BTW STA Y 160 TO STA Y 200 AND -X44 AT PASSENGER CABIN IN REF TO NRC 00392. SUMMARY OF NRC 00477: CORROSION LEVEL 2. NEW FLOOR SUPPORT BTW STA Y 160 TO STA Y 200 AND -X44 WAS REPLACED PER B717 SRM 51-41-02-0G, 51-41-05-0G PAR 8, AND DWG 9936534-71. (LP #0042355)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,454 hrs · 34,677 cycles

PUNCTURE ON DIAPHGRAM STA Y 155 X=7 AT PAX CABIN IN REF NRC 0395. W1. SUMMARY OF NRC 00561: DIAPHGRAM STA Y 155 X=7 AT PAX CABIN WAS REPAIRED PER B717 SRM 51-70-10-2R-2. (LP #0037357)

Part: POWER SUPPLY — DEFECTIVE (CABIN) · airframe 49,446 hrs · 34,673 cycles

THE AFT EXIT LIGHT IS MALFUNCTIONING BLINKING. MAINTENANCE REPLACED THE AFT POWER SUPPLY PER B717 AMM 33-51. OPERATION IS NOW NORMAL. (LP #7217374

Part: BATTERY — DISCHARGED (CABIN) · airframe 49,012 hrs · 34,329 cycles

THE AFT EMERGENCY EXIT SIGN, CAPTAINS SIDE, IS INOPERATIVE. MAINTENANCE FOUND THAT ALL OF THE ASSOCIATED LIGHTS WITH EMERGENCY POWER SUPPLY B5-260 WERE FLASHING IN THE ARMED POSITION. THE BATTERY AND BATTERY POWER SUPPLY WERE REPLACED PER AMM 33-51-03. ALL OPERATIONS ARE NOW NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 47,282 hrs · 33,063 cycles

THE AFT EXIT AND EMERGENCY LIGHTS IN THE CATWALK ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY AND CHARGED IT AT B-5260. LIGHTS NOW CHECK NORMAL PER AMM 33-51. (LP #5664562)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,500 hrs · 32,537 cycles

THE TAIL CONE EMERGENCY EXIT LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND THE CHARGER PER B717 AMM 33-51. CHECK WAS GOOD. (LP #3790932)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 45,950 hrs · 32,179 cycles

THE CAT WALK IN THE TAIL CONE LOWER EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY IN REAR OF AIRCRAFT AND THE CAT WALK EMERGENCY LIGHTS RETURNED TO NORMAL FUNCTION IAW B717 AMM 33-50. (LP #5174986)

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 45,228 hrs · 31,696 cycles

SURFACE CORROSION FOUND AT THE LT UPPER WING SKIN, STRINGER 5 LWS 343 TO 348.5. THE CORROSION WAS BEYOND THE LIMITS IAW SRM 57-10-01, ALLOWABLE DAMAGE 1.

Part: FRAME — CRACKED (BS 696) · airframe 45,198 hrs · 31,671 cycles

CRACK INDICATION GREATER THAN 0.125 INCH AT THE BS 696 FRAME TAB UPPER RADIUS. REPLACED THE FRAME IAW AMDS 5310-01436-03B.

Part: SLIDE — LOOSE (TAILCONE) · airframe 45,198 hrs · 31,671 cycles

TAILCONE SLIDE PACK WAS LOOSE AND UNRAVELED. INSTALLED A NEW TAILCONE SLIDE IAW AMM 25-61-02, AND AMDS CARD 5352-4002.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 44,285 hrs · 31,008 cycles

EMERGENCY CEILING LIGHTS ARE INOPERATIVE BETWEEN SEAT ROWS 1 AND 13. MAINTENANCE REPLACED THE BATTERY PACK IAW AMM 33-51-03. EMERGENCY LIGHT OPS NORMAL.

Part: DOOR FRAME — CRACKED (SERVICE DOOR) · airframe 40,249 hrs · 28,112 cycles

RIGHT FORWARD GALLEY SERVICE DOOR, LOWER FORWARD CORNER, LOWER HORIZONTAL FRAME CRACKED. REPLACED GALLEY SERVICE DOOR LOWER HORIZONTAL FRAME IAW SRM 51-41-02, 51-41-05, B DWG 5910084, REINSTALLED R1 DOOR IAW AMM 52-42-01 000-801, 52-42-01 400-801, PRESSURE CHECKED GOOD.

Part: SKIN — CORRODED (BS 1002) · corrosion level 2 · airframe 40,672 hrs · 28,455 cycles

SKIN CORRODED AFT OF BS 1002 ABOVE STRINGER 26. BLENDED AREA IAW SRM 53-00-00 FIG 103. FOUND TO BE OUT OF LIMITS. REPAIRED IAW ER/A 54713-14 REV O.

Part: DOOR FRAME — CRACKED (FUSELAGE) · corrosion level 2 · airframe 40,249 hrs · 28,112 cycles

AFT CARGO INTERNAL FUSELAGE CUT OUT, LOWER DOOR JAMB PAN HAS NUMEROUS AREAS OF CORROSION THAT IS AROUND THE AFT CAM LATCH FITTING AND LOWER AFT STOP ASSY TO THE FWD LOWER AFT STOP AND FWD CAM LATCH FITTINGS INCLUDING SPLICES. AROUND BARREL NUTS, AND THE 2 LOWER ANGLES, AFT ANGLE IS BENT AND CRACKED. AFT CARGO DOOR JAMB PAN WAS FOUND TO BE CRACKED AND CORRODED BEYOND LIMITS. ORIGINAL T=.050" REMAINING T=.000". THE OUT OF LIMITS PAN WAS REPLACED FROM THE AFT CARGO DOOR CUTOUT IAW SRM 53-20-15, REPAIR 7, THE SPLICE, 1 EA THAT WAS FOUND CORRODED SHOWED 100 PERCENT MATERIAL LOSS. THE NEW FWD DOOR JAMB SPLICE WAS FABRICATED IAW DWG J060228. IT WAS THEN ALODINED, PRIMED, AND PAINTED IAW AMM 51-10-00-370-803. THE NEW SPLICE WAS INSTALLED IAW SRM 51-41-02 & 51-41-05, ALSO ORNRC 70486-0100-0218 AND 70486-0100-0201.

Part: SEAL DEPRESSOR — DAMAGED (CARGO BAY) · corrosion level 2 · airframe 41,104 hrs · 28,813 cycles

FOUND AFT LOWER SEAL DEPRESSOR TO BE DAMAGED. COMPLIED WITH PRI 549608-14, AND ER/A 549608-14. BY FABRICATING PROTECTING & INSTALLATION OF AFT SEAL DEPRESSOR ON AFT CARGO DOOR CUTOUT.

Part: INTERCOSTAL — CORRODED (BS 1002-1022) · airframe 40,248 hrs · 28,111 cycles

FOUND INTERCOSTAL ABOVE LONGERON 28R, BS 1002-1022 TO BE CORRODED. REPLACED THE INTERCOSTAL IAW SRM 51-41-02 ORIGINAL, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00 FIG 103.

Part: SKIN — CRACKED (BS 1076) · airframe 40,248 hrs · 28,111 cycles

FUSELAGE SKIN CRACKED BS 1076 STRINGER 14R. REPAIRED THE SKIN IAW ER/A 547505-14.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,248 hrs · 28,111 cycles

STR 24 IS CORRODED AFT OF STA 1002. BLENDED AREA OF CORROSION FOUND TO BE OUT OF LIMITS, REMOVED .020 OF ORIGINAL .063 IAW SRM 53-00-00, FIG 103, TAG 2444. REPLACED LT 24R IAW SRM 51-41-02, PG 1-4 - 51-41-05, PG 1.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,248 hrs · 28,111 cycles

STR NR 23 IS CORRODED AFT OF STA 1002. BLENDED AREA OF CORROSION REMOVED L23R, .018 FROM ORIGINAL .063 FOUND TO BE OUT OF LIMITS IAW FIG 103, TAG 2444. REPLACED LT 23R IAW SRM 51-41-02, PG 1-4 AND SRM 51-41-05, PG 1.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,248 hrs · 28,111 cycles

STR 22 IS CORRODED AFT OF STA 1002. BLENDED AREA OF CORROSION ON LT 22R, REMOVED .015 OF ORIGINAL .063 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00, FIG 103. REPLACED LT 22R IAW SRM 51-41-02, PG 1-4 & 51-41-05 PG 1.

Part: SUPPORT ANGLE — CRACKED (L1 DOOR) · airframe 40,248 hrs · 28,111 cycles

SUPPORT ANGLE IS CRACKED INSIDE L1 DOOR FWD SIDE AT UPPER STOP. REPLACED SUPPORT ANGLE IAW SRM 51-41-02 PG 40 PARA B, 51-41-02 PG 1 PARA 4, AND 51-41-05 PG 17 PARA 8.

Part: CAP — CORRODED (BS 1002) · corrosion level 2 · airframe 40,248 hrs · 28,111 cycles

END CAPS ON STRINGER 24R AT BS 1002 CORRODED. BLENDED AREA OF CORROSION ON S24R END CAP. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00 FIG 103 REPLACED THE END CAP IAW ER/A 546907-14, SRM 51-41-05..

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 40,248 hrs · 28,111 cycles

AT STA 1152 LT LONGERON L1 FOUND SHEAR TIE CRACKED, MARKED. REPLACE REF ORNRC 70486-0200-0116. REPLACED SHEAR TIE IAW SRM 51-41-05.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,249 hrs · 28,112 cycles

RIGHT CUSP WEB AT STA 954 TO 1022 IS CORRODED OUT OF LIMITS. REPLACED RT CUSP WEB SECTION FROM STA 954 TO 1022 IAW DWG NR 9940158 AND SRM 53-00-55, REPAIR 4, FIG 212.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,248 hrs · 28,111 cycles

AFT CARGO FUSELAGE STA 1033 INTERCOSTAL ATTACHED TO STR 30 IS CORRODED. MARKED, BLENDED AND CHECK LIMITS, REPLACED AS REQUIRED, REF ORNRC 70486-0100-0162. REPLACED INTERCOSTAL AT FS 1022-1037 AT L30 IAW SRM 51-41-05. AFTER BLENDING CORROSION ON INTERCOSTAL IAW SRM 53-00-00, FIG 103. REMOVED .030 OF .063 BEYOND ALLOWABLE LIMITS, TAG 3310.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,248 hrs · 28,111 cycles

CORRODED ON STR 29L IN SEVERAL AREAS FROM STA 908-959 APPROXIMATELY. CLEAN, BLEND AND CHECK LIMITS 53-00-00, REF ORNRC 70486-0100-0119. BLENDED AREAS ON STR 29L FROM STA 908 TO 959, APPROXIMATELY .063 FROM ORIGINAL .080 FOUND TO BE IN LIMITS IAW SRM 53-00-00, FIG 103. ONE AREA AT STA APPROXIMATELY 910 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00, FIG 103, .063 OF ORIGINAL .125, REPAIRED IAW SRM 53-00-05, REPAIR 3. ALODINED, PRIMED AND TOP COATED BLENDED AREAS AND REPAIR PIECE IAW AMM 51-10-00 370-003 UT TOOL TAG 6784 & 6785.

Part: FRAME — GOUGED (BS 636) · airframe 40,248 hrs · 28,111 cycles

LEFT FUSELAGE FRAME BS 636 LWR END AROUND FASTENER IS GOUGED AND CRACKED. REPLACED THE IAW SRM 51-41-02, 51-41-05, & 51-40-08.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,248 hrs · 28,111 cycles

F/O AFT OTBD SEAT TRACK IS CORRODED. REPLACED SEAT TRACK IAW 51-41-01, PARA 2.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,248 hrs · 28,111 cycles

CORROSION ON THE UPPER AND LOWER SURFACES OF THE UPPER CUSP ANGLE, STA 219, RBL 58 AS VIEWED FROM THE CABIN AND THE UPPER FWD CORNER OF THE FORWARD CARGO RT SIDE TUNNEL. REPAIRED CUSP ANGLE IAW SRM 53-00-55, REPAIR 3.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,248 hrs · 28,111 cycles

FLC CORROSION STA 446, SHEAR TIE BETWEEN S29R AND 30. FLC FOUND CORROSION AT STA 446, SHEAR TIE BETWEEN L29R AND L30. CORROSION CLEANED AND BLENDED IAW SRM 53-00-00, FIG 103. ORIGINAL THICKNESS 0.063, 0.031 FOUND REMAINING OUT OF LIMITS. SHEAR TIE REPAIRED IAW SRM 53-00-06, REPAIR 3. REPAIR DOUBLER FABRICATED IAW SRM 53-20-07, FIG 1, ITEM 4 AND SRM 53-20-06, REPAIR 1, FIG 201. HEAT TREATED TO 7075-T6, MWO 70487-0018. T-ANGLE COMMON TO INTERCOSTAL AND FORMER AT STA 446, L29R REQUIRES REPLACEMENT DUE TO DOUBLER. FABRICATED IAW DWG 2913743, REV B. REPLACED IAW SRM 51-41-05.

Part: SHEAR TIE — CORRODED (BS 927) · corrosion level 2 · airframe 40,672 hrs · 28,455 cycles

FRAME AND SHEAR TIE CORRODED AT BS 927 BETWEEN STRINGERS 28L AND 28R. REPAIRED DAMAGE IAW SRM 53-20-06 AND 53-00-06 FIG 201 REPAIR 2. SRM 51-10-04 PAR 24.

Part: SEAT TRACK — CORRODED (BS 200-256) · corrosion level 2 · airframe 40,672 hrs · 28,455 cycles

SEAT TRACK RBL.56 BS 200 - 256 IS CORRODED. BLENDED AREA AND FOUND TO BE IN LIMITS ORIGINAL THICKNESS .100 REMOVED .010 REMAINING .090 IAW SRM 53-20-52 FIG 101. CORRODED END FITTING WAS REPLACED ON ORNRC 70486-0200-072 ITEM 7.

Part: CUSP WEB — CORRODED (BS 160-200) · corrosion level 2 · airframe 40,248 hrs · 28,111 cycles

CUSP WEB CORRODED BEYOND LIMITS AT BS 160 - 200, RBL 56. REPLACED THE CUSP WEB IAW ER/A 547507-14 REV A, SRM 51-41-02 AND 51-41-05.

Part: STRUCTURE — CORRODED (BS 200) · corrosion level 2 · airframe 40,248 hrs · 28,111 cycles

CORROSION ON THE UPPER AND THE LOWER SURFACES OF THE CABIN SUB FLOOR, BS 200, FWD AND AFT OF THE FLOORBEAM, FROM BL 0 TO RBL 58. REPLACED THE SUB FLOOR IAW ER/A 547507-14 REV A, SRM 51-41-02 AND 51-41-05.

Part: FLOOR SUPPORT — CORRODED · airframe 40,248 hrs · 28,111 cycles

FLOOR SUPPORT BRACKET FOR PANEL 221EF IS CORRODED. BLENDED FLOOR SUPPORT FOUND TO BE OUT OF LIMITS. FABRICATED, ALODINE, PRIMED, TOP COATED, AND INSTALLED A NEW FLOOR SUPPORT.

Part: SHEAR TIE — CRACKED (BS 1022) · airframe 40,248 hrs · 28,111 cycles

FOUND CRACKED SHEAR TIE AT BS 1022 RIGHT APPROXIMATELY 14 STRINGER. FABRICATED A NEW SHEAR TIE IAW DWG #9912243. INSTALLED THE SHEAR TIE IAW SRM 51-41-05 PARA 2.

Part: SEAT TRACK — GOUGED (BS 215-275) · airframe 40,248 hrs · 28,111 cycles

LEFT SEAT TRACK LBL 44.5 IS CORRODED AND GOUGED IN SERVERAL AREAS FROM BS 215 - 275. BLENDED AND CHECKED LIMITS. REPLACED THE SEAT TRACK IAW SRM 53-20-52 REPAIR 5.

Part: SEAT TRACK — CORRODED (BS 225-275) · corrosion level 2 · airframe 40,248 hrs · 28,111 cycles

LEFT INBD SEAT TRACK LBL 22 IS CORRODED AND GOUGED IN SEVERAL AREAS FROM BS 225 - 275. THE SEAT TRACK WAS REPLACED IAW SRM 53-20-52 CONFIGURATION 700, AND SRM 51-10-04 PARA 9 & 10.

Part: SEAT TRACK — CORRODED (BS 200-256) · corrosion level 2 · airframe 40,248 hrs · 28,111 cycles

SEAT TRACK RBL 44.5 BS 200 - 256 IS CORRODED. REPLACED THE SEAT TRACK IAW SRM 51-41-01, 51-41-02, 53-20-52 REPAIR 5.

Part: DOOR FRAME — CORRODED (FWD CARGO) · corrosion level 2 · airframe 40,248 hrs · 28,111 cycles

LOWER FUSELAGE, FWD CARGO DOOR FRAME HAS MULTIPLE AREAS OF CORROSION. THE DOOR FRAME WAS REPLACED REPLACED IAW SRM 53-20-15 REP 6.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 40,248 hrs · 28,111 cycles

CUSP WEB CRACKED AT RT STA 218-237. REPLACED CUSP AT F/S 218-237 IAW SRM 51-41-02, PARA D, NOTE 3. FASTENERS THROUGH SEAT TRACKS TO BE INSTALLED ON ORNRC 0200-0172, PARTIAL 2.9, ORNRC 0200-0164.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 40,248 hrs · 28,111 cycles

LEFT CUSP WEB CRACKED AROUND LIGHTNING HOLE, STA 664, LBL 46. REPLACED WITH NEW CUSP WEB IAW SRM 51-41-02.

Part: CUSP WEB — CRACKED (BS 222) · airframe 40,248 hrs · 28,111 cycles

LEFT CUSP WEB CRACKED AT BS 222 LBL 44.5. REPAIRED IAW SRM 53-00-55 REPAIR 4.

Part: SEAT TRACK — CORRODED (BS 986-1053) · corrosion level 2 · airframe 40,248 hrs · 28,111 cycles

LEFT CENTER SEAT TRACK, LBL 44.5, BS 986 - 1053 CORRODED. SEAT TRACK BLENDED AND FOUND TO BE OUT OF LIMITS IAW SRM 40-20-50. REPLACED THE SEAT TRACK SECTIONE. FABRICATED IAW DWG 9981474 AND ER/A 547506-14-REV A.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,248 hrs · 28,111 cycles

CORROSION ON SKIN AT STA 1212.225 L30 FOUND TO BE OUT OF LIMITS, REF ORNRC 7046-0100-0041. INSTALLED REPAIR DOUBLER IAW SRM 53-02-01, REPAIR 1, FIGURE 202 AT STA 1212.225 L30.

Part: PAN — CRACKED (CARGO DOOR) · airframe 40,248 hrs · 28,111 cycles

CRACKED INTERIOR STRUCTURE OF THE FWD CARGO DOOR, LWR FWD AREA. REPAIRED THE DOOR PAN IAW CMM 52-30-01 PG D601.1.

Part: STRUCTURE — CRACKED (CARGO DOOR) · airframe 40,248 hrs · 28,111 cycles

CRACK ON INTERIOR STRUCTURE OF THE FWD CARGO DOOR LWR AFT AREA. REPAIRED IAW OVERHAUL MANUAL 52-30-1.

Part: PIN — MISINSTALLED (TAILCONE RELEASE) · airframe 39,788 hrs · 27,718 cycles

THE TAILCONE FAILED TO DEPLOY DURING ROUTINE DROP TEST. MAINTENANCE DISCOVERED THAT THE RELEASE LATCH T-PIN NR 12 FOR THE TAILCONE WAS NOT PROPERLY ENGAGED. THE T-PIN WAS REENGAGED AS DESIGNED AND IN COMPLIANCE WITH AMDS 5352-2001 THE SYSTEM WAS RIGGED TO SPECIFICATIONS. THE RII AND FUNCTIONAL CHECK WAS COMPLETED SATISFACTORILY.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 35,539 hrs · 24,286 cycles

RIGHT FWD OVERWING EMER EXIT SIGN LOWER BULB INOPERATIVE. R & R BULB IAW AMM.

Part: PANEL — CRACKED (LT WING) · airframe 35,391 hrs · 24,189 cycles

LEFT WING INBD BUTTE DOOR INBD END AT AFT HINGE, INBD CORNER PANEL CRACKED. REPAIR PANEL IAW SRM & EA.

Part: BATTERY PACK — FAILED (CABIN) · airframe 35,391 hrs · 24,189 cycles

RIGHT EMER LIGHT FAILED CHECK. R & R BATTERY PACK ASSEMBLY IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 35,391 hrs · 24,189 cycles

LEFT EMER LIGHT FAILED CHECK. R & R BATTERY PACK ASSEMBLY IAW AMM.

Part: BATTERY — INOPERATIVE (CABIN) · airframe 35,391 hrs · 24,189 cycles

EMERGENCY LIGHT BATTERY BASE FOUND INOPERATIVE. R & R BATTERY BASE IAW AMM.

Part: LIGHT — INOPERATIVE (TAILCONE) · airframe 35,391 hrs · 24,189 cycles

TAIL CONE EMER LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: FAIRING — CRACKED (RT HORIZ STAB) · airframe 35,391 hrs · 24,189 cycles

RIGHT HORIZONTAL STABILIZER UPPER BANANA FAIRING CRACKED. R & R FAIRING IAW AMM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 35,391 hrs · 24,189 cycles

FLOOR SUPPORT CORRODED AT BS 220, BETWEEN LONGERON 13L TO 10R. R & R SUPPORT IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 35,391 hrs · 24,189 cycles

FORWARD WET AREA FLOOR SUPPORT CORRODED BETWEEN STATION 200 X-9 TO STATION 200 X-45. R & R FLOOR SUPPORT IAW SRM.

Part: ATTACH FITTING — CORRODED (GIRT BAR) · airframe 35,391 hrs · 24,189 cycles

R1 DOOR EMER EVAC SLIDE FWD GIRT BAR ATTACH FITTING CORRODED. R & R FITTING IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 35,391 hrs · 24,189 cycles

FORWARD GALLEY FLOOR SUPPORT CORRODED AT STATION 196-200 X+59. R & R FLOOR SUPPORT IAW SRM.

Part: ATTACH FITTING — CORRODED (GIRT BAR) · airframe 35,391 hrs · 24,189 cycles

R1 DOOR EMER EVAC SLIDE AFT GIRT BAR ATTACH FITTING CORRODED. R & R FITTING IAW SRM & DWG.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 35,391 hrs · 24,189 cycles

AFT CARGO DOOR JAM CORRODED AT LOWER SECTION BETWEEN BS 954 TO 963. REPAIRED JAM IAW SRM & DWG.

Part: DOOR — CRACKED (LT WING) · airframe 35,391 hrs · 24,189 cycles

LEFT WING INBD BUTTE DOOR INBD END AT AFT HINGE INBD CORNER CRACKED. REPAIRED DOOR IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,959 hrs · 22,025 cycles

FRAME AT STA 737 RT IS CRACKED BELOW CUSP WELL. ACCOMPLISHED EA 17-53-03955.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 30,718 hrs · 21,195 cycles

UPON REMOVAL OF CUSP WEB LEFT STA 655 - 718 FOUND MULTIPLE CRACKS IN WEB. REPAIRED WEB PER SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 30,718 hrs · 21,195 cycles

UPON REMOVAL OF RIGHT CABIN CUSP MEMBRANE FROM STA 655 TO 718 NUMEROUS CRACKS WERE FOUND UNDER GUSSETS FOR FRAME CUT OUTS. CUT OUT DAMAGE 3 AREAS ON RIGHT CUSP WEB PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 31,959 hrs · 22,025 cycles

FLOORBEAM WEB AT STA 674, LBL 55 IS CRACKED BETWEEN CHANNEL AND FITTING. ACCOMPLISHED EA 17-53-03956.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 30,718 hrs · 21,195 cycles

FLOORBEAM WEB CRACKED AT BS 674, LBL 55. REMOVED AND REPLACED WEB PER IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,718 hrs · 21,195 cycles

RIGHT FRAME AT STA 715 IS CRACKED AT I/B RADIUS, UNDER CUSP WEB. REMOVED AND REPLACED FRAME AT STA 715 LONGERON 9R-18R IAW EA 17-53-04005.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 30,718 hrs · 21,195 cycles

UPON REMOVAL OF CUSP WEB STA 715 TO 756 LEFT SIDE - FOUND CRACKED AT CORNER CUTOUT AFT END OF CUSP WEB. CUT OUT DAMAGE ON CUSP WEB 1 1/4" X 5/8 IAW B717 SRM 53-00-55 REPAIR 4 FIG 212 FABRICATED FILLER FROM 7075-T6 .040 X 1 1/14X 5/8 PO 9001497

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 30,718 hrs · 21,195 cycles

CUSP WEB CRACKED BETWEEN BS 715 TO BS 756 LEFT SIDE. REPAIRED WEB IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,718 hrs · 21,195 cycles

FRAME CRACKED AT BS 737 RT. REMOVED AND REPLACED FRAME IAW SRM.

Part: RUB STRIP — CORRODED (RT WING) · airframe 30,718 hrs · 21,195 cycles

RIGHT AFT WING TO BODY FAIRING RUB STRIP AT L-25R IS CORRODED. PRIMED EXPOSED MATERIAL ON LEFT WING FWD L/E OF VORTION IAW B717 SRM 51-10-04 PG 19-20 PAR 15.

Part: LIGHT — CORRODED (RT WING) · airframe 30,718 hrs · 21,195 cycles

RIGHT WING UPPER SURFACE - 620FT LANDING LIGHT CORRODED. REMOVED AND REPLACED LIGHT IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,718 hrs · 21,195 cycles

SEAT TRACK SECTION CORRODED BETWEEN BS 588 TO BS 899, LBL 54.6. REMOVED AND REPLACED SEAT TRACK IAW SRM.

Part: STRAP — CRACKED (CARGO BAY) · airframe 30,718 hrs · 21,195 cycles

AFT LOWER CARGO COMPARTMENT FWD BULKHEAD PANEL ATTACH STRAP CRACKED BS 817, BL 0 TO LBL 28, 15" ABOVE PIT FLOOR. REMOVED AND REPLACED AFT CARGO FWD BLUKHEAD STRAP FOR PANEL ATTACHMENT IAW B717 SRM 51-41-02, 51-40-08 AND MD DWG 5956040.

Part: STRAP — CRACKED (CARGO BAY) · airframe 30,718 hrs · 21,195 cycles

LOWER CARGO COMPARTMENT BULKHEAD GILLINER ATTACH STRAP CRACKED AT BS 817, RBL 16 TO RBL 35. REMOVED AND REPLACED STRAPS IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,718 hrs · 21,195 cycles

SEAT TRACK SECTION CORRODED BS 899 TO BS 589, RBL 54.6. REMOVED AND REPLACED TRACK IAW SRM.

Part: BRACKET — CRACKED (RT WING) · airframe 30,718 hrs · 21,195 cycles

RIGHT WING L/E - THE MOST I/B BRACKET CRACKED AT STA XCW 59. REMOVED AND REPLACED RIGHT WING L/E BONDING STRAPS IAW B717 SRM 51-41-02,51-40-08 AND MD DWG 5919110.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 30,718 hrs · 21,195 cycles

CABIN FLOOR PANEL 222 AAF DELAMINATED. REMOVED AND REPLACED PANEL IAW AMM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 30,718 hrs · 21,195 cycles

CABIN FLOOR PNL 221 WF IS DELAMINATED. REMOVED AND REPLACED MAIN CABIN FLOOR PANEL 221WF IAW B717 AMM 53-21-01. REPLACEMENT PANEL FABRICATED IAW B717 SRM 53-20-50 REPAIR 3 AND FIG 1.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 30,718 hrs · 21,195 cycles

CABIN FLOOR PANEL 222 LF DELAMINATED. REMOVED AND REPLACED PANEL IAW AMM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 30,718 hrs · 21,195 cycles

CABIN FLOOR PNL 221 DF HAS DELAMINATION. REMOVED AND REPLACED MAIN CABIN FLOOR PANEL 221PF IAW B717 AMM 53-21-01. FABRICATED FLOOR PANEL REPLACEMENT IAW B717 SRM 53-20-50 REPAIR 3 AND FIG 1.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 30,718 hrs · 21,195 cycles

CABIN FLOOR PNL 222JF HAS DELAM. REMOVED MAIN CABIN FLOOR PNL 222JF IAW B717 AMM 53-21-0 FABRICATED FLOOR PNL FROM PN# B227002 TYPE 3 PO# 79019953 DIM 21" X 76" IAW B717 SRM 53-20-50 REPAIR 3 INSTALLED FLOOR PNL 222JF IAW B717 SRM 51-41-01.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 30,718 hrs · 21,195 cycles

CABIN FLOOR PANEL 222 ABF DELAMINATED. REMOVED AND REPLACED PANEL IAW AMM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 30,718 hrs · 21,195 cycles

CABIN FLOOR PNL 222 RF IS DELAMINATED. REMOVED AND REPLACED MAIN CABIN FLOOR PNL 222RF IAW B717 AMM 53-21-01. REPLACEMENT FLOOR PANEL FABRICATED IAW B717 SRM 53-20-50 REPAIR 3 AND FIG 1.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 30,718 hrs · 21,195 cycles

CABIN FLOOR PNL 221 UF HAS DELAMINATION. REMOVED AND REPLACED CABIN FLOOR PANEL 221UF IAW B717 AMM 53-21-01. FABRICATED REPLACEMENT PANEL IAW B717 SRM 53-20-50 REPAIR 3 AND 53-20-50 FIG 1.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 30,718 hrs · 21,195 cycles

CABIN FLOOR PNL 222 ACF IS DELAMINATED. REMOVED AND REPLACED CABIN FLOOR PNL 222ACF IAW B717 AMM 53-21-01. REPLACEMENT PANEL FABRICATED IAW B717 SRM 53-20-50 EREPAIR 3 AND FIG 1.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 30,718 hrs · 21,195 cycles

CABIN FLOOR PANEL 222 AGF DELAMINATED. REMOVED AND REPLACED PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 30,718 hrs · 21,195 cycles

CABIN FLOOR PNL 222FF IS DELAMINATED. REMOVED AND REPLACED MAIN CABIN FLOOR PANEL 222FF IAW B717 AMM 53-21-01. FABRICATED FLOOR PANEL IAW 53-20-50 REPAIR 3 AND FIG 1.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 30,718 hrs · 21,195 cycles

CABIN FLOOR PANEL 222 APF IS DELAMINATED. REMOVED CABIN FLOORBOARD 222ADF IAW B717 AMM 53-21-01 FABRICATED FLOOR PANEL IAW B717 SRM 53-20-50 + DWG. INSTALLED FLOOR PANEL IAW B717 SRM 51-41-01.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 30,718 hrs · 21,195 cycles

CABIN FLOOR PNL 222 PF HAS DELAM. REMOVED MAIN CABIN FLOOR PNL 222PF IAW B717 AMM 53-21-01 FABRIACTED FLOOR PNL FROM PN BZZ7002TYPE3 PO# 790191094 DIM 21"X76" IAW B717 SRM 53-20-50 REPAIR 3 INSTALLED FLOOR PNL 222PF IAW B717 SRM 51-41-01.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 30,718 hrs · 21,195 cycles

CABIN FLOOR PANEL 222 AHF IS DELAMINATED. REMOVED DELAMINATED CABIN FLOOR PNL 222AHF IAW B717 AMM 53-21-01 FABRICATED FLOOR PANEL SRM 53-20-52 REPAIR 3 + DWG, INSTALLED FLOOR PNL IAW B717 SRM 51-41-01.

Part: INTERCOSTAL — CRACKED (L1 DOOR) · airframe 30,718 hrs · 21,195 cycles

L1 DOOR INTERNAL STRUCTURE BRACKET CRACKED SIDE DOOR. REMOVED AND REPLACED INTERCOSTAL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 30,718 hrs · 21,195 cycles

CABIN FLOOR PANEL 222AMF DELAMINATED. REMOVED AND REPLACED PANEL IAW AMM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 30,718 hrs · 21,195 cycles

CABIN FLOOR PNL 222 BF HAS DELAMINATION. REMOVED AND REPLACED MAIN CABIN FLOOR PANEL 222BF IAW B717 AMM 53-21-01. REPLACEMENT PANEL FABRICATED IAW B717 SRM 53-20-50 REPAIR 3 AND FIG 1.

Part: PAN — CORRODED (FUSELAGE) · airframe 30,718 hrs · 21,195 cycles

CARGO DOOR CUTOUT LOWER PAN CORRODED BETWEEN BS 954 TO BS 980. REMOVED AND REMOVED PAN IAW SRM.

Part: LIGHT — MISSING (CABIN) · airframe 30,978 hrs · 21,378 cycles

EEPLS BULBS MISSING BETWEEN ROW 14 TO ROW 16. INSTALLED BULBS PER MM.

Part: LENS — MISSING (CABIN) · airframe 30,978 hrs · 21,378 cycles

EEPLS LENSES MISSING BETWEEN ROW 14 TO ROW 16. INSTALLED LENSES PER MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 30,844 hrs · 21,283 cycles

FORWARD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER AMM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 29,784 hrs · 20,582 cycles

RT OVERHEAD EMERGENCY EXIT LIGHT INOP AT ROW 22. REMOVED AND REPLACED BATTERY SUPPLY ASSY PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 29,788 hrs · 20,585 cycles

RT OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: COVER — LOOSE (EVAC SLIDE) · airframe 29,782 hrs · 20,580 cycles

L1 DOOR EMERGENCY EVAC SLIDE COVER LOOSE. SECURED COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN)

THE RED LIGHT AT THE EMERGENCY EXIT ROW DOES NOT ILLUMINATE. RE-LAMPED EMERGENCY EXIT LIGHT AS REQUIRED.

Part: LIGHT — MISSING (CABIN)

THE 10D ESCAPE PATH LIGHTING COVER AND BULB MISSING. RELAMPED & INSTALLED LENS COVER 25-23.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY EXIT ROWS 11-19 LIGHTS OUT (SEAT LIGHTS). REMOVED AND REPLACED EMERGENCY LIGHT BATTERY AND POWER SUPPLY IAW AMM 33-51-03. ALSO RE-PINNED POWER WIRE COMING IN AT ROW 15 IAW WPM 33-51 SYSTEM, OPS CHECKED GOOD.

Part: COVER — MISSING (CABIN)

THE 23D EMERGENCY ESCAPE PATH LIGHTING ON SEAT BASE IS MISSING ITS COVER. REINSTALLED COVER, OPS CHECK OK MM 33-51.

Part: COVER — MISSING (CABIN)

SEAT 20D EXIT ROW RED LIGHT COVER MISSING. REPLACED SEAT 20D RED LIGHT COVER OPS CHECKS NORMAL REF MM 33-24.

Part: SEAT — SMOKE (COCKPIT)

ON APPROACH HEARD A SIZZLING SOUND AND SMOKE SEEPING FROM BEHIND CAPT CHAIR. NO CIRCUIT BREAKERS WERE POPPED. UPON ARRIVAL AT A/C SMELLED NO UNUSUAL ODORS. FOUND NO CIRCUIT BREAKERS IN COCKPIT POPPED. OPENED CIRCUIT BREAKER PANEL BEHIND / CAPTAIN SEAT AND FWD F/A'S SEAT AND INSPECTED AREAS FOR EVIDENCE OF ARCING OR LOOSE CONNECTORS AND FOUND NONE. CHECKED E&E / BAY AND FWD ACCESSORY AND FOUND NO RELATED DEFECTS. RAN AC PACK WITH APU AND ENGINE AND SMELLED NO UNUSUAL ODORS. FOUND / EMPTY COOKIE CONTAINER WEDGED BEHIND CAPTAINS SEAT. COOKIE CONTAINER IS SUSPECTED SOURCE OF SIZZLING / SOU. WORK DONE PER 717 FAULT ISOLATION MANUAL 21-22. CHIEF INSPECTOR NOTIFIED AS REQUIRED. A/C OK FOR SERVICE.

Part: COVER — MISSING (CABIN)

ROWS 19, 23 AND 27 EMERGENCY LENS COVERS MISSING. INSTALLED LENS COVERS AT ROWS 19, 23 AND 27 EMERGENCY LIGHTS REF: B717 AMM 33-51-04. OK FOR SERVICE.

Part: SIGN — BROKEN (CABIN)

CEILING EXIT SIGN IN MIDDLE OF AIRCRAFT IS BROKEN. RE-ASSEMBLED SIGN, OPS NORMAL REF MM 33-50.

Part: STRUCTURE — CRACKED (LT PYLON)

LEFT PYLON APRON LOWER NR 2 HINGE CUT OUT AREA, CRACKED. ACCOMPLISHED NR 2 HINGE CUTOUT AREA DOUBLER REPAIR PER TRA 17-54-TR00129.

Part: PAN — CORRODED (FUSELAGE)

FWD CARGO DOOR JAMB PAN, STA 370 TO 427, CORROSION. ACCOMPLISHED JAMB PAN SPLICE REPAIR PER B717 SRM 53-20-15 FIG 201 REPAIR 6.

Part: WEB — CORRODED (FUSELAGE)

CABIN FLOOR WEB, STA 200, RBL 44, CORROSION. ACCOMPLISHED FLOOR WEB DOUBLER REPAIR PER B717 SRM 51-41-02.

Part: STRUCTURE — CRACKED (LT PYLON)

LEFT PYLON APRON UPPER AFT HINGE CUTOUT, CRACKED. ACCOMPLISHED AFT HINGE CUTOUT DOUBLER REPAIR PER TRA 17-54-TR00129.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT ANGLE, STA 149 TO 200, RBL 54, CORROSION. ACCOMPLISHED FLOOR SUPPORT ANGLE REPLACEMENT PER B717 SRM 51-41-02.

Part: DOOR FRAME — CRACKED (FUSELAGE)

PASSENGER ENTRANCE AREA DOOR JAMB WEB, STA 206, LONG L15L, CRACKED. ACCOMPLISHED DOOR JAMB WEB DOUBLER REPAIR PER B717 SRM 51-70-10 FIG 201 REPAIR 2.

Part: LENS — DAMAGED (CABIN)

RED LENS ON EMERGENCY LIGHTING SYSTEM SEAT NR 21D. RELAMPED AND INSTALLED NEW LENS COVER ON EMERGENCY LIGHT AT SEAT 21D IAW AMM 33-51. OPS CHECKED GOOD. OK FOR SERVICE.

Part: COVER — OUT OF POSITION (EXIT SIGN)

FORWARD AISLE CEILING MOUNTED EXIT SIGN PLASTIC COVER FELL OFF. TEMPORARILY SECURED EXIT SIGN AND PLACED ON NEF.

Part: COVER — MISSING (FUSELAGE)

THE 22D RED COVER MISSING ON ESCAPE PATH LIGHTS. INSTALLED RED LENS, CHECKED LIGHT OPERATION REF 33-51.

Part: LIGHT — BROKEN (CABIN)

ESCAPE PATH LIGHT AT SEAT 15D LENS MISSING, ONE BULB BROKEN. INSTALLED LENS AND RELAMPED ASSY REF 33-51-04.

Part: SLIDE — LOW PRESSURE (R1 DOOR)

F/A REPORTED R1 DOOR ESCAPE SLIDE PRESSURE IS LOW. REPLACED R1 DOOR ESCAPE SLIDE PER MM 25-61-03.

Part: FRAME — CORRODED (FUSELAGE)

AFT CARGO COMPARTMENT CENTER BILGE FRAME 974 HAS CORROSION L 29L AND L 29R - OUT OF LIMITS. INSTALLED ROLLED Z-FRAME REPAIR SPLICE IAW B717 SRM 58-20-07 FIG 201 REP 3.

Part: STRUCTURE — CRACKED (AFT CARGO DOOR)

AFT CARGO DOOR FWD LOWER EDGE AREA IS CRACKED. INSTALLED PERMANENT REPAIR AT LOWER EDGE DIMENSION 7 X 3 INCHES PER B717 SRM 52-30-02.

Part: BULKHEAD — DAMAGED (FUSELAGE)

DAMAGE (HOLE) IN FWD CARGO COMPARTMENT BULKHEAD. INSTALLED TYPICAL WEB TRIM OUT REPAIR DOUBLER PER B717 SRM 51-70-10 REP 2.

Part: PAN — CORRODED (FUSELAGE)

AFT CARGO COMP DOOR CUTOUT LOWER DOOR JAM CORRODED OUT OF LIMITS. INSTALLED NEW AFT CARGO DOOR LOWER PAN & SPLICE REPAIR PER B717 SRM 53-20-15.

Part: WIRE — DAMAGED (EMERGENCY LIGHT)

EMERGENCY LIGHTS INOP ON ROW 25-30. REPAIRED WIRING (EMERGENCY TRACK PATH) REF SWPM 20-10 AT SEAT 25. OPS CK GOOD REF MM 33-51.

Part: LINE — LEAKING (NR 1 ENGINE)

INFLIGHT ENGINE SHUTDOWN AFTER LOSS OF OIL PRESSURE. INSPECTED NR 1 ENGINE IAW AMM 72-00-00-200-805, TIGHTENED B-NUT ON OIL PUMP PRESSURE DISTRIBUTION LINE IAW AMM 79-20-00; OPS CHECK GOOD. RAN NR 1 ENGINE AT TAKEOFF POWER IAW AMM 71-00 TEST NR 2A, NO LEAKS NOTED.

Part: SEAL — LOOSE (BULLET)

N1 VIBRATION ON RIGHT ENGINE INCREASED OVER TIME FROM 4.0 TO 7.0 AT 310. ON DESCENT VIBRATION TO 9.0 AND WAS FELT THROUGHOUT AIRCRAFT. ICING IN CLIMB, ENGINE ONLY NO WING OR TAIL. TEMP AT 310 - 40 C. ENGINE ONLY ICE WAS USED. REMOVED AND REPLACED AIR INTAKE ROTATING FAIRING AND NOSE IAW B717 AMM 72-38-01, OPS CHECKS NORMAL. RAN ENGINE VIB WITHIN LIMITS, OK FOR SERVICE. FOUND OMEGA SEAL ON OLD NOSE CONE SEPARATED FROM SPINNER, REF 52EB03.