N949AT

Part: APU — ODOR (ZONE 100) · airframe 64,161 hrs · 46,222 cycles

SHIP 9500 DIRTY SOCKS SMELL WITH APU AIR ON WHEN TAKING OVER THE AIRPLANE. CORECTIVE ACTION: R/R APU REF B717 AMM 49-10 (7813574)

Part: COVER — UNSECURE (BATTERY) · airframe 64,161 hrs · 46,222 cycles

SHIP 9500 ROW 19C & 19D EMERGENCY BATTERY COVER LOOSE. CORECTIVE ACTION: RE-SECURED AS REQUIRED (7813580)

Part: WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 63,912 hrs · 45,990 cycles

SHIP 9500 AFT CARGO DOOR THRESHOLD WEB CORRODED SEVERAL LOCATIONS AT UPPER AND LOWER SURFACES. CORRECTIVE ACTION: REMOVED AND REPLACED WEB PER B717 DWG 5910158 (1055786)

Part: NOT ENTERED — NO DISCREPANCY (NOT REPORTED) · airframe 63,912 hrs · 45,990 cycles

9500 REPETITIVE INSP PER SECT II. OF ERA 627055-14 REV A. CORRECTIVE ACTION: ACCOMPLISH SECTION II: REPETITIVE INSPECTIONS EVERY EIGHT THOUSAND (8,000) FLIGHT CYCLES FROM ACCOMPLISHMENT OF SECTION I: PERMANENT REPAIR PER ER/A 627055-14 REV A. (1055040)

Part: SKIN — DAMAGED (ZONE 100) · corrosion level 2 · airframe 64,552 hrs · 46,572 cycles

AFT CARGO DOOR AND DOOR FRAME: FUSELAGE SKIN DOOR CUTOUT AREA AFT EDGE DAMAGED. C/W AFT CARGO CORROSION ERA 627055-14 REV A. (1055785)

Part: SKIN — BENT (ZONE 800) · airframe 63,912 hrs · 45,990 cycles

AIRCRAFT 9500, FWD CARGO DOOR AND DOOR FRAME: DOOR SKIN BENT ALONG LOWER EDGE. CORRECTIVE ACTION: REPAIRED PER B717 SRM 52-00-01-2R-8. (LP 1011857)

Part: SPAR CAP — CRACKED (ZONE 500) · airframe 63,912 hrs · 45,990 cycles

SHIP 9500 LH WING REAR SPAR LOWER CAP CRACK. REPAIRED PER ERA 623615-14AD REV 0 (0990246)

Part: REPAIR — NOT REPORTED · airframe 63,912 hrs · 45,990 cycles

SHIP 9500 EXISTING REPAIR FOUND PER ERA 623617-14AD REV ORIG. CORRECTIVE ACTION: REPAIRED PER 623617-14AD (0986223)

Part: SPAR CAP — CRACKED (ZONE 500) · airframe 63,912 hrs · 45,989 cycles

-AD- LEFT WING REAR SPAR LOWER CAP IB OF FLAP TRACK. CRACK INDICATION IN HOLE THAT IS 2 HOLES IB OF EXISTING CRACK, XRS 164. REF PRI 621050-14 REV 1 STEP 11 AND FIGURE 3. SUMMARY SEE NRC 006-0001:10-0557-8-8910/002 00039: REFERENCED PRI 621050-14 ALL REVISIONS ISSUED FOR NR 17. C/W WITH PRI 621050-14 REV 0, REV 1, REV 2, REV 3, REV 4, REV 5, REV 6, REV 7, REV 8, REV 9, REV 10, REV 11, AND ERA 621050-14 REV ORIGINAL, REV A. CLOSING REQUIREMENTS RII: INSPECTOR 00528138. (LP #0740556)

Part: SPAR — CRACKED (ZONE 500) · airframe 63,912 hrs · 45,989 cycles

-AD- VISIBLE CRACK FOUND ON LEFT WING REAR SPAR LOWER CAP IB OF FLAP TRACK, OB OF THE TE RIB CLIP BETWEEN XRS 150.450 AND XRS 164.000. SUMMARY SEE NRC 006-0001:10-0557-8-8910/001 00017: COMPLIED WITH PRI 621050-14 REV 0, REV 1, REV 2, REV 3, REV 4, REV 5, REV 6, REV 7, REV 8, REV 9, REV 10, REV 11, AND ERA 621050-14 REV ORIGINAL, REV A. (LP #0740554)

Part: NONE — NONE (NONE) · airframe 63,912 hrs · 45,989 cycles

-AD- WHILE IN MAINTENANCE, AA WORK CARD 5720-01103-01B RH WING XRS 164, REAR SPAR AND LWR SKIN INSPECTION WAS COMPLETED WITH NO FINDINGS. DAL BELIEVES ADDITIONAL INSPECTIONS BEYOND THE SCOPE OF AA WC 5720-01103-01B ARE NECESSARY TO VERIFY NO DAMAGE IS PRESENT IN THE REAR SPAR AND LOWER SKIN OF THIS A/C. THIS ER /A PROVIDES ADDITIONAL INSTRUCTIONS TO INSPECT THE RH WING REAR SPAR WING SKIN AND FORWARD FACE OF THE SPAR CAP. SUMMARY SEE NRC 003-0002:1270-2999/001 00052: COMPLIED WITH PRI 621526-14AD REV 0, REV 1, REV 2, REV 3, REV 4, REV 5, REV 6, AND FINAL ERA 621526-14AD REV ORIGINAL. CLOSING REQUIREMENTS RII: INSPECTOR 00528138. CLOSING REQUIREMENTS RII: INSPECTOR 00528138. (LP #0740544)

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 63,657 hrs · 45,787 cycles

FOUND L & R FWD OVERWING EXIT EMERGENCY LIGHTS TO BE INOPERATIVE. ALSO FOUND L & R FWD SERVICE DOOR EXIT EMERGENCY LIGHTS INOPERATIVE. PER B717 WDM 33-51-14, ALL LIGHTS ASSOCIATED WITH BATTERY PACK B5-118. REPLACED EMERGENCY LIGHT BATTERY PACK B5-118 IAW B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. OK FOR SERVICE. (LP #6185107)

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 63,546 hrs · 45,693 cycles

CEILING PANEL 6,7,8, AND MID CABIN OVERHEAD EXIT LIGHT INOPERATIVE. MAINTENANCE REPLACED #5 EMERGENCY BATTERY PACK PER B717 FRMFIM 33-50. OPERATIONAL CHECK WAS GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME. (LP #6057526)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,373 hrs · 45,530 cycles

THE EMERGENCY LIGHT IN CEILING PANELS FROM ROW 2 TO ROW 11 ARE INOPERATIVE. MAINTENANCE FOUND THE EMERGENCY BATTERY #5 B5-227 TO BE INOPERATIVE PER B717 FRMFIM 33-50. THE #5 EMERGENCY BATTERY WAS REPLACED PER AMM 33-51. OPERATIONAL CHECK WAS GOOD. NO FURTHER DEFECTS NOTED.

Part: FLOOR PANEL — GOUGED (FWD CARGO) · airframe 63,337 hrs · 45,497 cycles

FWD CARGO FLOOR PANEL HAS GOUGE AND UPPER SURFACE CRACKED. REPAIRED FLOOR PANEL 121NF FWD CARGO IAW B717-200, SRM 53-20-50-2R, ACCOMPLISH PERMANENT REPAIR WITHIN 500 FLIGHT HOURS PARTS REQUIRED 9936599-501 PANEL OR MATERIAL S00096. REDEFERRED LOG TO QC, ESTAB MON INSP. REMOVED FWD CARGO FLOOR PANEL 121NF PER B717 AMM 25-58-01 ON 19JUN24. INSTALLED FWD CARGO FLOOR PANEL 121NF PER B717 AMM 25-58-01 ON 20JUN24. CLOSED LOG AND REMOVED MONITOR INSP. (LP #0285905)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 61,727 hrs · 44,114 cycles

SHIP 9500 -ATB- THE AIRCRAFT WAS RETURNED TO ATL FOLLOWING COMPRESSOR SURGES IN THE #1 ENGINE. THE PILOT DECLARED AN EMERGENCY WITH ATC AND THE LANDING & TAXI TO THE GATE WAS UNEVENTFUL. CORRECTIVE ACTION: MAINTENANCE REPLACED THE #1 ENGINE (ESN 13197) AND THE AIRCRAFT WAS RETURNED TO SERVICE. (LP #9635642)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 61,559 hrs · 43,968 cycles

FOUND TAIL SLIDE CONTAINER OPEN AND SLIDE UNPACKED. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. REPLACED TAILCONE SLIDE PER B717 W/C 2561-9006. ALL RII STEPS ACCOMPLISHED PER W/C 2561-9006. (LP #4465331)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 60,416 hrs · 42,952 cycles

SHIP 9500 -ATB- THE CREW DECLARED AN EMERGENCY AND RETURNED THE AIRCRAFT MYR DUE THE #2 BRAKE OVER TEMPERATURE WARNING ILLUMINATING. QRH PROCEDURES FAILED TO LOWER THE TEMPERATURE INDICATION. THE LANDING WAS UNEVENTFUL AND THE AIRCRAFT BRAKING WAS NORMAL. CORRECTIVE ACTION: MAINTENANCE FOUND THE #2 BRAKE TEMPERATURE SENSOR BROKEN IN HALF AND REPLACED IT. (LP #4076698)

Part: UNKNOWN — UNKNOWN · airframe 60,398 hrs · 42,938 cycles

THE FORWRD EMERGENCY OVERWING LIGHTS ARE INOPERATIVE. MAINTENACE REPLACED THE EMERGENCY BATTERY POWER SUPPLY B5-118 IAW B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #4076686)

Part: UNKNOWN — UNKNOWN · airframe 60,398 hrs · 42,938 cycles

THE OVERHEAD EMERGENCY LIGHT OVER THE CATWALK IS INOPERATIVE. MAINTENACE REPLACED THE POWER SUPPLY B5-116 REF B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. OK FOR SERVICE. (LP #4076685)

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 59,925 hrs · 42,545 cycles

SEVERAL DENTS ON LOWER SKIN OF RT WING FLAP FIXED VANE, THE SKIN WAS REPAIRED IAW SRM 57-53-01-2R-1, AND SRM 51-70-02-0G.

Part: VANE — DAMAGED (RT WING TE FLAP) · airframe 59,925 hrs · 42,545 cycles

DURING TAP-TEST INSPECTION OF DENTS AT RHS FWD MOVABLE VANE, A DISBONDED AREA OF 4.750 IN LENGTH AND 2.000 IN WIDTH WAS FOUND ON THE RUB STRIP. RT FWD MOVABLE VANE WAS REPAIRED IAW SRM 51-70-02-0G PAR. 15, 17A, AND SRM 57-53-01-2R-1 PAR. 4 D.

Part: SUPPORT RIB — WORN · airframe 59,925 hrs · 42,545 cycles

WORN INBD RIB SUPPORT ON FIXED LEADING EDGE WS XRS 267.000 APPROX AT RH WING. AD. SUMMARY OF NRC 00166: INBD RIB SUPPORT ON FIXED LEADING EDGE WS XRS 267.000 APPROX AT RH WING WAS REPAIRED PER ER/A 604521-14 REV ORIGINAL SECTION 1 PERMANENT REPAIR AND PRI 604521-14 REV 0. ASSOCIATED ER/A 14-604521 ADDED FOR AC 9500. (LP #2547299)

Part: FRAME — CORRODED (BS 974 L29-30R) · airframe 59,925 hrs · 42,545 cycles

CORROSION AT FRAME STA Y=974 BTW LONGERON 29R-30 AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00223: LEVEL CORROSION 2. FRAME STA Y=974 BTW LONGERON 29R-30 WAS REPAIRED PER B717-200 SRM 53-20-07-0G REPAIR 3. (LP #2544348)

Part: FRAME ANGLE — PUNCTURED (BS 908 L29-30R) · airframe 59,925 hrs · 42,545 cycles

PUNCTURE ON FRAME CLIP STA Y=908 BTW LONGERON 29R-30 AFT CARGO COMPARTMENT (C2) IN REF 00227. SUMMARY OF NRC 00261: FRAME CLIP WAS REPLACED PER B717-200 SRM 53-20-07-0I. (LP #2544352)

Part: DOOR FRAME — CORRODED (BS 954 L2627R) · corrosion level 2 · airframe 59,925 hrs · 42,545 cycles

CORROSION ON AFT CARGO COMPARTMENT DOOR JAMB REPAIR DOUBLER AT STA Y=954 BTW LONGERON PROJECTION 27RH AND 26RH. SUMMARY OF NRC 00138: CORROSION LEVEL 2. AFT CARGO COMPARTMENT DOOR JAMB REPAIR DOUBLER AT STA Y=954 BTW LONGERON PROJECTION 27RH AND 26RH WAS REPLACED PER B717-200 SRM 53-20-15-2R-7 PAR. 5.A. TABLE 201 REPAIR 7. ITEM 33, SRM 51-41-05-0G AND SRM 51-41-01-0G. (LP #2543742)

Part: SKIN — CRACKED (BS 1087 L5R) · airframe 59,925 hrs · 42,545 cycles

CRACK ON EXTERNAL SKIN ABOVE LONGERON 15 RH AND STA 1087 AT FUSELAGE. SUMMARY OF NRC 00026: CRACK ON EXTERNAL SKIN ABOVE LONGERON 15 RH AND STA 1087 AT FUSELAGE WAS REPAIRED PER PRI 604254-14 REV 4 AND PER ER/A 604254-14 REV ORIGINAL, SECTION I: PERMANET REPAIR. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING ACCOMPLISH SECTION II NOT TO EXCEED EVERY 24 MONTHS AFTER ACCOMPLISHMENT OF SECTION I PERMANENT REPAIR. ASSOCIATED ER/A 14-604254 ADDED FOR AC 9500. (LP #2543488)

Part: DOOR FRAME — CORRODED (BS 370-427) · corrosion level 2 · airframe 59,925 hrs · 42,545 cycles

CORROSION ON LOWER DOOR JAMB EXTRNAL SURFACE FROM STA 370 TO 427 AT FWD CARGO COMPARTMENT (CCD). SUMMARY LEVEL CORROSION 2. DOOR JAMB EXTRNAL SURFACE FROM STA 370 TO 427 WAS REPLACED PER B717-200 51-40-08-0G PAR 3 AND SRM 51- 41-02-0G AND 51-41-05-0G. (LP #2543797)

Part: PAN — CRACKED · airframe 59,925 hrs · 42,545 cycles

CRACK ON UPPER PAN WAS FOUND IN REFERENCE NRC 0063. SUMMARY OF NRC 00256: CRACK ON UPPER PAN WAS REPAIRED PER B717- 200 SRM 52-10-02-2R PROCEDURE 3 REPAIR 3. (LP #2539972)

Part: BEAM — CRACKED · airframe 59,925 hrs · 42,545 cycles

CRACK OF AFT EDGE OF BEAM NO 1 AT STA Y=199 AT FWD PASSENGER DOOR. (L1) SUMMARY OF NRC 00063: CRACK OF AFT EDGE OF BEAM NO 1 AT STA Y=199 WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 7 REPAIR 7. (LP #2539977)

Part: SKIN — CRACKED (PAX DOOR) · airframe 59,925 hrs · 42,545 cycles

CRACK ON LOWER EDGE OF FWD PASSENGER DOOR EXTERNAL SKIN BS 167. EXTERNAL SKIN STA Y=167 OF LOWER EDGE AT FWD PASSENGER DOOR (L1) WAS REPAIRED PER B717-200 SRM 52-10-01- 2R REPAIR 1 PROCEDURE 1 PAR. 4.

Part: FLOORBEAM — CRACKED · airframe 59,925 hrs · 42,545 cycles

A CRACK WAS FOUND IN FLOORBEAM STA 735 X=-58 AT WING BOX AREA (WB), WHILE PERFORMING AMDS 5310-01436-01C. SUMMARY OF NRC 00249: BEAM STA 735 X=-58 AT WING BOX AREA (WB) WAS REPLACED PER B717-200 SRM 51-41-03-0G PAR 11, 51-41-02-0G, 51-41-01-0G, 51-41-02-0G PAR. 4, 51-41-05-0G PAR.8, AND 51-41-08-0G PAR.7. (LP #2536134)

Part: FLANGE — CORRODED (RT MLG) · airframe 59,786 hrs · 42,422 cycles

RIGHT MLG FIXED STRUT I/B FITTING BUSHING I/B FLANGE PITTED (MKD). SUMMARY NRC 004-0003:3211-4002/003 00003: REPAIRED BUSHING AND BORE PER BOEING OHM 57-40-1, REPAIRED I/B AND O/B FACES PER ERA 603437-14 REV O. (LP #2479152)

Part: BATTERY PACK — INOPERATIVE · airframe 58,789 hrs · 41,543 cycles

THE CEILING EMERGENCY LIGHTS FROM ROW 1 TO 19 ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACKS B5-227 AND B5-120 REF B717 AMM 33- 51. OPERATIONAL CHECK IS GOOD. THE AIRCRAFT IS OK FOR SERVICE. (LP #8549167)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,899 hrs · 39,883 cycles

THE FLIGHT DECK OVERHEAD EMERGENCY LIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK B5-123 PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #7808348)

Part: SKIN — CORRODED (FUSELAGE) · airframe 55,798 hrs · 39,004 cycles

BULGE FOUND IN FUSELAGE SKIN BENEATH AFT CARGO COMPARTMENT JUST AFT OF Y STATION 1022.091 AND AT LONGERON R29- MARKED. COMPLIED WITH PRI 589616-14 REV O-2, REPAIRED REF ER/A 589616-14 REV B. SEE NRC 34. (LP #1718582)

Part: SKIN — CORRODED (BS 1022 S29R) · airframe 57,927 hrs · 40,788 cycles

DTA REQUIRED FOR ER/A 589616-14 REV B / FUSELAGE / SKIN / STA 1022 / L-29R / SKIN BULGE. DTE REQUIRED FOR ER/A 589616-14 REV B. REPAIR APPROVAL IS LIMITED TO 12 MONTHS ONLY. ADDITIONAL ENGINEERING AUTHORIZATION (ER/A REVISION) IS REQUIRED FOR CONTINUED SERVICE BEYOND THIS LIMIT. NOTE TO ENGINEER: DAMAGE TOLERANCE ANALYSIS IS REQUIRED IN ACCORDANCE WITH PROCEDURES ESTABLISHED IN FAA AC 120-93. ASSOCIATED ER/A 00-589616 ADDED FOR AC 9500. ERA 589616-14 REV C IS CURRENT. REF NEW LP 2075336, THIS LP MAY BE CLOSED. (LP #1717813)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,724 hrs · 38,031 cycles

ON WAKE-UP CHECK, THE TWO FORWARD OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED SAME PER AMM 33-51. OPERATIONAL CHECK WAS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,724 hrs · 38,031 cycles

THE OVERWING EMERGENCY EXIT IDENTIFIER LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK B5-119 PER AMM 33-51-03. OPERATIONAL CHECK IS NORMAL.

Part: TERMINAL — BROKEN (EMERGENCY LIGHT) · airframe 54,244 hrs · 37,673 cycles

THE AFT CATWALK CEILING CENTER EMERGENCY LIGHT IS INOPERATIVE. MAINTENANCE FOUND BOTH POWER/GROUND TERMINALS BROKEN. RETERMINATED TERMINAL WIRES REF B717 WDM 33-51-13. OPERATIONAL CHECK GOOD. (LP #6669500)

Part: COVER — DISENGAGED (TAILCONE SLIDE) · airframe 53,022 hrs · 36,780 cycles

THE TAIL CONE SLIDE COVER WAS FOUND TO BE DISENGAGED. THE SLIDE ASSEMBLY, SN 1571RP, WAS INSPECTED AND THE COVER WAS CLEARED TO BE RE-INSTALLED. INSTALLED SLIDE PER B717 WORKCARD 2561- 9006, STEPS 6-10. ALL RII COMPONENTS WERE SATISFIED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (LP #5949596)

Part: WINDOW FRAME — CRACKED · airframe 51,880 hrs · 35,911 cycles

CRACK ON UPPER AFT CORNER CLEAR VIEW WINDOW FRAME LH SIDE. (CPIL). NRC 00390: UPPER AFT CORNER WINDOW OPENING LH SIDE WAS REPAIRED PER B717-200 SRM 56-10-02-2R REPAIR 1, ER/A 575163-14 REV. ORIG., AND ETI-17-19-015 REV. ORIG. ASSOCIATED ER/A 00-575163 ADDED FOR AC 9500. (LP #0935767)

Part: VANE — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 51,921 hrs · 35,949 cycles

CORROSION ON LH AFT MOVABLE FLAP VANE AT LH FLAP. (AI). NRC: 00140 CORROSION LEVEL II, CORROSION WAS FOUND OUT OF LIMITS PER B717-200 SRM 57-53-02-0I-1 ITEM 1 AND SRM 57-00-00-1A FIGURE 103. AFT LH MOVABLE FLAP VANE WAS REPLACED PER B717-200 AMM 27-50-03 400-802 AND ADJUSTED PER B717-200 AMM 27-50-03 200-801. TOOL USED TENSIOMETER P/N: T5-2002-101-00, S/N: 74721, D/D: 16JUN19. THERMOMETER P/N: TM360, S/N: QT-1024, D/D: 22FEB19. (LP #0935354)

Part: WINDOW — CRACKED (COCKPIT) · airframe 51,880 hrs · 35,911 cycles

CRACK ON UPPER AFT CORNER CLEAR VIEW WINDOW RT SIDE. UPPER AFT CORNER CLEAR VIEW WINDOW RT SIDE WAS REPAIRED PER SRM 56-10-02-2R REPAIR 1, ER/A 575163-14 REV ORIG, AND ETI-17-19-015 REV ORIG.

Part: SKIN — GOUGED (FUSELAGE) · airframe 51,880 hrs · 35,911 cycles

GOUGES AND NICKS ON FUSELAGE SKIN FROM STA Y1109 TO Y1129 BTW LONGERONS 12L-14L (FUS). FUSELAGE SKIN FROM STA Y1109 TO Y1129 BTW LONGERONS 12L-14L WAS REPAIRED PER ER/A 575178-14 REV ORIG AND ETI-17-19-017 REV 3.

Part: VANE — WORN (FLAP) · airframe 51,880 hrs · 35,911 cycles

WEAR ON AFT MOVABLE FLAP VANE LEADING EDGE 1 INCH FROM OUTBD EDGE (AD). NRC 00085: AFT MOVABLE FLAP VANE LEADING EDGE WAS REPAIRED PER B717 SRM 57-53-01-2R PROCEDURE 1 REPAIR 1 AND S.R.M. 51-70-02-0G. (LP #0930248)

Part: PIN — OUT OF POSITION (TAILCONE) · airframe 51,880 hrs · 35,911 cycles

TAILCONE SLIDE CAM PIN WAS FOUND WITH THE WRONG ORIENTATION. (IN REF 5352-4002). CAM PIN WAS ADJUSTED (ORIENTATED) CORRECTLY PER AMM 53-52-03 820-801.

Part: DOOR FRAME — CORRODED (BS 954-994) · corrosion level 2 · airframe 51,880 hrs · 35,911 cycles

CORROSION ON LOWER DOOR JAMB FROM STA Y=954 TO Y=994 AT AFT CARGO COMPARTMENT. (C2). NRC 00253: CORROSION LEVEL 2, DOOR JAM FROM STA Y=954 TO Y=994 AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #0926752)

Part: CARGO TRACK — CORRODED (BS 908-954) · corrosion level 2 · airframe 51,880 hrs · 35,911 cycles

CORROSION ON RH TIE TRACK FROM STA Y=908 TO Y=954 AT AFT CARGO COMPARTMENT (AMDS 5331-2001). (CCT). NRC 00376: CORROSION LEVEL 2, SECTION ON RH TIE TRACK FROM STA Y=908 TO Y=954 AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-05-0G AND 51-41-02-0G. (LP #0926695)

Part: CUSP WEB — CRACKED (BS 579-589) · airframe 51,880 hrs · 35,911 cycles

CRACKS ON CUSP-MEMBRANE RH SIDE BETWEEN STA 579-589. (CPAX). NRC 00241: CUSP-MEMBRANE RH SIDE BETWEEN STA 579-589 WAS REPLACED PER B717-200 SRM 51-41-02-0G. (LP #0926077)

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,880 hrs · 35,911 cycles

CORROSION ON LT CUSP WEB STA 889-908 IN PAX CABIN IN REF NRC 00238. NRC 00477: CORROSION LEVEL 2, CUSP WEB LT BTW STA 889-908 AT PAX CABIN WAS REPLACED PER SRM 51-41-02-0G. (LP #0925509)

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,880 hrs · 35,911 cycles

SEVERAL CORRODED AREAS ON PREVIOUS DOUBLER REPAIR SPLICE ON STA Y=954 AND Y=994 AT AFT CARGO COMPARTMENT. (C2). NRC 00254: CORROSION LEVEL 2, DOUBLERS REPAIR SPLICE ON STA Y=954 AND Y=994 AT AFT CARGO COMPARTMENT WERE REPLACED PER SRM 53-20-15-2R-7. (LP #0924021)

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,880 hrs · 35,911 cycles

CORROSION OUT OF LIMITS ON CUSP-MEMBRANE RT SIDE BETWEEN STA 560-636 IN REF NRC 00240. NRC 00481: CORROSION LEVEL 2, WEB WAS REPLACED PER SRM 53-00-55-2R-4 FIG 226 AND 51-41-02-0G. (LP #0923003)

Part: VANE — DELAMINATED (TE FLAP) · airframe 52,082 hrs · 36,072 cycles

DURING TAP TEST INSPECTION PER SRM 57-53-01-1A PARA 2. B DELAMINATION OF 1.625" X 0.750" WAS FOUND AT DENT NR 1 LOCATED 22" OUTBD AND 5" T/E. IN REF JOB #70. NRC 00504: FORWARD MOVABLE OUTBD VANE WAS REPAIRED PER SRM 51-70-02-0G PARAGRAPH 15. A AND SRM 57-53-01-2R PROCEDURE 1 REPAIR 1 PARAGRAPH 4. (LP0921360)

Part: FORMER — CRACKED (RT MLG WW) · airframe 51,880 hrs · 35,911 cycles

CRACKED FORMER ON RT MLG FWD DOOR JAMB OUTBOARD SECTION (FYT). NRC 00184: FORMER WAS REPLACED PER SRM 51-41-05-0G AND SRM 51-41-02-0G. (LP #0920939)

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 51,880 hrs · 35,911 cycles

CRACKS ON CUSP-MEMBRANE LT SIDE BETWEEN STA 655-674 AND 696-715. (CPAX). NRC 00239: WEB WAS REPLACE PER SRM 53-00-55-02R-4 FIG 226. (LP #0921069)

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 51,880 hrs · 35,911 cycles

CORROSION ON RT TIE TRACK FROM STA Y-588 TO Y-653 AT FWD CARGO COMPARTMENT (CCD). NRC 0323: CORROSION LEVEL 2, RT TIE TRACK FROM STA Y-588 TO Y-653 AT FWD CARGO COMPARTMENT WAS REPLACED PER SRM 51-41-01-0G AND 51-41-02-0G. (LP #0919720)

Part: FITTING — CRACKED (FUSELAGE) · airframe 51,880 hrs · 35,911 cycles

CRACKED CLIP ON STA Y=655 X=0 AT WINGBOX (WB). NRC 0273: CLIP WAS REPLACED PER SRM 51-41-05 AND DWG #S1103715 REV. A. (LP #0920065)

Part: BEAM — CRACKED (FUSELAGE) · airframe 51,880 hrs · 35,911 cycles

CRACK BEAM #6 BTW STA 172-190 AT PASSENGER ENTRANCE DOOR L1 (PTAS). NRC 00380: BEAM #6 WAS REPAIR PER ER/A 559578-14MA REV. ORIGINAL. ASSOCIATED ER/A 17-559578 ADDED FOR AC 9500. (LP #0916770)

Part: ACCESS PANEL — CORRODED (WIING) · corrosion level 2 · airframe 51,880 hrs · 35,911 cycles

CORROSION ON HOLE AT FUEL ACCESS PANEL #520LB, 520CB, 620PB, AND FUEL PANEL P/N ARB 0975-17-9. NRC 00444: CORROSION LEVEL 2, FUEL ACCESS PLATES WERE REPAIRED PER SRM 57-10-01 REPAIR 2 PAR. 5 CONDITION II. (LP #0916148)

Part: ANGLE — CRACKED (FUSELAGE) · airframe 51,880 hrs · 35,911 cycles

CRACKED ANGLE ON INTERCOSTAL FROM STA Y=409 TO 407 UPPER BEAM AT FWD CARGO DOOR (C-1) IN REF NRC: 00102. NRC 00505: ANGLE WAS REPLACED PER SRM 51-41-02-0G. (LP #0916065)

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 51,880 hrs · 35,911 cycles

CORROSION ON SEVERAL HOLES AT FUEL ACCESS PANELS #620FT, 620AT, 620CT, 520CT, 141AL, 141AR, AND FUEL PANEL P/N ARB 0975-17. NRC 00445: CORROSION LEVEL 2: FUEL ACCESS PANELS #620FT, 620AT, 620CT, 520CT, 141AL, 141AR, AND FUEL PANEL P/N ARB 0975-17 WERE REPLACED PER SRM 57-10-01 REPAIR 2 PAR 5 CONDITION III. (LP #0916157)

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 51,880 hrs · 35,911 cycles

CRACK INTERCOSTAL FROM STA Y=409 TO Y=407 UPPER BEAM AT FWD CARGO DOOR. (C-1). NRC 00102: INTERCOSTAL FROM STA Y=409 TO Y=407 UPPER BEAM AT FWD CARGO DOOR WAS REPLACED PER SRM 51-41-02-0G, 51-41-05-0G, 51-41-04-0G, AND DWG #9957664 REV N. (LP #0916062)

Part: FORMER — CRACKED (FUSELAGE) · airframe 51,880 hrs · 35,911 cycles

CRACKED LT FORMERS STA Y:660.0, Y:675.5, & Y:696.0 AT UNDERWING BARREL CANTED KEEL BEAM AREA (FUS). NRC 0389: LT FORMERS STA Y:660.0, Y:675.5, & Y:696.0 WERE REPAIRED PER SRM 51-70-11-2R -1 REPAIR 1 FIG. 201. (LP #0916479)

Part: PAN — CRACKED (FUSELAGE) · airframe 51,880 hrs · 35,911 cycles

CRACK ON OUTBOARD PAN IN STA Y=370 AND Y=427 BEAM 3 AT FWD CARGO DOOR. (C-1). NRC 00101: CRACKS ON OUTBOARD PAN IN STA Y=370 AND Y=427 BEAM 3 WERE REPAIRED PER SRM 52-30-02-2R REPAIR 1 FIG. 201, SRM 51-41-01-0G, SRM 51-41-02-0G AND 51-41-04-0G. (LP #0916806)

Part: FITTING — CRACKED (FUSELAGE) · airframe 51,880 hrs · 35,911 cycles

CRACKED FRAME CLIP ON CENTER WING STA Y=715 XCW=44 AT WINGBOX (WB). NRC 00270: FRAME CLIP (CAP) ON CENTER WING STA Y=715 XCW=44 AT WINGBOX WAS REPLACED PER SRM 51-41-05-0G AND 51-41-01-0G. (LP #0916509)

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 51,880 hrs · 35,911 cycles

DELAMINATION AND DAMAGED FERRULES AT PAX CABIN FLOOR PANELS #222CF, 221VF, 223CF, AND 221BF (CPAX). NRC 00452: FLOOR PANELS #222CF, 221VF, 223CF, AND 221BF WERE FABRICATED, REPLACED, AND IDENTIFIED PER SRM 53-20-50-2R-3. (LP #0914549)

Part: LONGERON — CRACKED (FUSELAGE) · airframe 51,880 hrs · 35,911 cycles

CRACK ON LONGERON 17L AT STA. 1022.091. (CPAX). NRC 00303: LONGERON 17L BTW STA: 955 TO STA: 1053 WAS REPLACE PER SRM 51-41-02-0G AND SRM 51-41-05-0G. (LP #0914172)

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,880 hrs · 35,911 cycles

CORROSION OUT OF LIMITS ON CUSP-MEMBRANE RT SIDE BETWEEN STA 385-389 IN REF NRC 00240. NRC 00479: CORROSION LEVEL 2, CUSP-MEMBRANE RT SIDE BETWEEN STA 385-389 WAS REPAIRED PER SRM 53-00-55-2R-4 FIG 224. (LP #0910963)

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 51,880 hrs · 35,911 cycles

CRACK INTERCOSTAL BETWEEN BEAM 5 AND 4 STA 186 AT PASSENGER ENTRANCE DOOR L1 (PTAS). NRC 00381: INTERCOSTAL WAS REPLACED PER SRM 51-41-02-0G PAR. 6 B, 51-41-01-0G, AND DWG #9955763 REV. K. (LP #0912023)

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,880 hrs · 35,911 cycles

CORROSION ON LT CUSP WEB STA 874-883 AT PAX CABIN IN REF NRC 00238 IS OUT OF LIMITS. NRC 00476: CORROSION LEVEL 2, CUSP WEB STA 874-883 AT PAX CABIN WAS REPAIRED PER SRM 53-00-55-2R-4. (LP #0910970)

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,880 hrs · 35,911 cycles

CORROSION ON LT CUSP WEB STA 864-870 AT PAX CABIN IN REF NRC 00238 IS OUT OF LIMITS. NRC 00475: CORROSION LEVEL 2, CUSP WEB STA 864-870 WAS REPAIRED PER SRM 53-00-55-2R. (LP #0910951)

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,880 hrs · 35,911 cycles

CORROSION OUT OF LIMITS ON CUSP-MEMBRANE RT SIDE BETWEEN STA 496-500 IN REF NRC 00240. NRC 00480: CORROSION LEVEL 2, CUSP-MEMBRANE RT SIDE BETWEEN STA 496-500 WAS REPAIRED PER SRM 53-00-55-2R-4 AND 51-41-02-0G. (LP #0910461)

Part: DRIVE ASSY — DAMAGED (LE SLAT) · airframe 48,560 hrs · 33,590 cycles

THE CREW EXPERIENCED AN UN-COMMANDED ROLL WHEN THEY SELECTED THE SLATS TO EXTEND. MAINTENANCE FOUND THAT THE RIGHT WING INBOARD LEADING EDGE SLAT DRIVE WAS DAMAGED. THE DRIVE WAS REPLACED AND A FUNCTIONAL TEST FLIGHT WAS ACCOMPLISHED.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 47,684 hrs · 32,969 cycles

VERTICAL STAB LEADING EDGE BELOW ZFS 52, HAS 53 ELONGATED FASTENER HOLES. COMPLIED WITH PRI 559269-14 REV 0 AND ER/A 559269-14AD REV ORIGINAL.

Part: SCREW — LOOSE (VERTICAL STAB) · airframe 47,684 hrs · 32,969 cycles

VERTICAL STAB LEADING EDGE APPROX STA ZFS 52, FOUR ROWS SPLICE 40 SCREWS LOOSE. SEE NR FOR ADDITIONAL INFORMATION 001-0235:5530-2005/003 00123 REPAIR PER SRM55-30-01-2R-6. FPI PER PS 900-6-3 NR 02.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 47,167 hrs · 32,582 cycles

DURING A SERVICE CHECK, FOUND THE MID CABIN LOWER EMERGENCY EXIT SIGNS INOPERATIVE. TROUBLESHOT THE EMERGENCY LIGHTS IAW FIM 33-50-00 810-801. R & R THE BATTERY PACK IAW 33-51. OPS CHECKED NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 46,180 hrs · 31,884 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING FOR THE TAIL COMPARTMENT WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS AND THE OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 44,737 hrs · 30,687 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGN FOR THE FWD OVERWING HATCH WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. OPS CHECK WAS GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 43,102 hrs · 29,371 cycles

AFT EMER FLASHLIGHT INOPERATIVE. R & R BATTERY ASSEMBLY IAW AMM.

Part: WIRE — MISROUTED (AC BAY) · airframe 43,102 hrs · 29,371 cycles

TAIL COMPARTMENT EMER OVERHEAD LIGHT WIRE MISROUTED. REROUTED WIRE IAW SRM.

Part: LIGHT — INOPERATIVE (AC BAY) · airframe 43,102 hrs · 29,371 cycles

TAIL COMPARTMENT CATWALK FIRST EMER LIGHT BULB INOPERATIVE. R & R BULB IAW AMM.

Part: LIGHT — INOPERATIVE (AC BAY) · airframe 43,102 hrs · 29,371 cycles

TAIL COMPARTMENT CATWALK AFT HANDRAIL EMER LIGHT BULB INOPERATIVE. R & R BULB IAW AMM.

Part: LIGHT — INOPERATIVE (AC BAY) · airframe 43,102 hrs · 29,371 cycles

TAIL COMPARTMENT CATWALK AFT EMER LIGHT BULB INOPERATIVE. R & R BULB IAW AMM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

AFT PIT FITTING CRACKED AT BS 1002, LONGERON 28R. R & R FITTING IAW DWG.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

CABIN FLOOR SUPPORT CRACKED AT BS 200, LBL 20. R & R SUPPORT IAW SRM & DWG.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 42,611 hrs · 29,026 cycles

AFT CARGO COMPARTMENT TRACK CORRODED BETWEEN BS 992 - 1022, BETWEEN LONGERON 27R - 28R. R & R TRACK IAW DWG.

Part: FORMER — CRACKED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

FORMER CRACKED AT BS 1152, LONGERON 2R. R & R FORMER IAW SRM & DWG.

Part: FORMER — CRACKED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

AFT ACCESSORY COMPARTMENT FORMER CRACKED AT BS 1152, LONGERON 2L. REPAIRED FORMER IAW SRM & DWG.

Part: SKIN — CORRODED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

AFT CARGO COMPARTMENT LOWER DOOR CUT OUT SKIN CORRODED AT BS 974. REPAIRED SKIN IAW EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 43,106 hrs · 29,372 cycles

AFT CARGO COMPARTMENT LOWER DOOR SKIN CUT OUT CORRODED AT BS 974. REPAIRED SKIN IAW EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 43,106 hrs · 29,372 cycles

AFT CARGO COMPARTMENT LOWER DOOR CUT OUT SKIN CORRODED AT BS 974. REPAIRED SKIN IAW EA.

Part: FORMER — CRACKED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

FORMER CRACKED AT BS 1116, LONGERON 16L. R & R FORMER IAW SRM.

Part: MEMBRANE — CORRODED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

MAIN CABIN MEMBRANE WEB CORRODED AT STATION 202, RBL 7. REPAIRED MEMBRANE WEB IAW SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

AFT CARGO COMPARTMENT INTERIOR SKIN CORRODED BETWEEN BS 954 - 964, BETWEEN LONGERON 27R - 29R. REPAIRED SKIN IAW EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

SHEAR TIE CORRODED AT BS 946, BETWEEN LBL 28 TO LBL 27. R & R SHEAR TIE IAW SRM.

Part: MEMBRANE — CRACKED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

MAIN CABIN MEMBRANE CRACKED AT BS 200, LBL 17. REPAIRED MEMBRANE IAW SRM.

Part: MEMBRANE — CRACKED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

MAIN CABIN FWD WET AREA MEMBRANE CRACKED AT BS 218, RBL 46. R & R MEMBRANE IAW SRM.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

FORWARD CARGO COMPARTMENT RT TUNNEL CORRODED BETWEEN BS 500 - 515, BETWEEN LONGERON 20R - 19R. R & R TUNNEL IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

MAIN CABIN FLOOR SUPPORT CORRODED AT BS 200, RBL 7. R & R SUPPORT IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

MAIN CABIN WEB CRACKED AT BS 210, LONGERON 15L. REPAIRED WEB IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

FUSELAGE FRAME CLIP CRACKED AT STATION 1053, LT SIDE. R & R CLIP IAW SRM.

Part: FORMER — CORRODED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

KEEL BEAM FORMER CORRODED AT BS 696, BETWEEN LONGERON 30R TO 26R. R & R FORMER IAW DWG.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

CABIN SEAT TRACK SUPPORT CRACKED AT STATION 737, LBL 44. R & R SUPPORT IAW DWG.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

AFT PRESS BULKHEAD DOUBLER CORRODED BETWEEN STRINGER 29R - 29L. R & R DOUBLER IAW DWG.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

CABIN SEAT TRACK SUPPORT CRACKED AT STATION 737, RBL 44. R & R SUPPORT IAW DWG.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

CENTER WING TANK FLOOR SUPPORT CRACKED AT BS 655, BL 0. R & R SUPPORT IAW SRM & DWG.

Part: DOUBLER — CRACKED (LT WING) · airframe 42,611 hrs · 29,026 cycles

LEFT WING FIXED LE SKIN DOUBLER CRACKED AT INBD SIDE OF VORTILON. REPAIRED SKIN DOUBLER IAW SRM.

Part: MEMBRANE — CORRODED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

MAIN CABIN MEMBRANE CORRODED AT BS 200, RBL 51. REPAIRED MEMBRANE IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

RIGHT WING TO BODY SUPPORT FRAME CORRODED AT BS 832 LOWER END. R & R FRAME IAW DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

MAIN CABIN FLOOR SUPPORT CORRODED BETWEEN BS 200 TO 157, RBL 55. R & R SUPPORT IAW SRM & DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

AFT CARGO DOOR JAMB AREA, AFT WEB CORRODED BETWEEN BS 992 TO 1002, BETWEEN LONGERON 23R TO 28R. R & R WEB IAW DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

SHEAR TIE CORRODED AT BS 1022, BETWEEN LONGERON 30 - 29L. R & R SHEAR TIE IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

MAIN CABIN FLOOR SUPPORT CORRODED BETWEEN BS 200 TO 150, LBL 44. R & R SUPPORT IAW DWG & SRM.

Part: FORMER — CORRODED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

FRAME SHEAR TIE HAS CORRODED AT BS 927, BETWEEN LONGERON 29L TO 29R. REPAIRED FORMER IAW SRM.

Part: MEMBRANE — CORRODED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

MAIN CABIN MEMBRANE CORRODED AT BS 157, RBL 32. REPAIRED MEMBRANE IAW SRM.

Part: FORMER — CRACKED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

MAIN CABIN FORMER CRACKED AT BS 1022, LONGERON 14R. REPAIRED FORMER IAW EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

SHEAR TIE CORRODED AT BS 908, BETWEEN LONGERON 28R - 29L. R & R SHEAR TIE IAW SRM.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

LONGERON CORRODED BETWEEN BS 899 - 1012, LONGERON 30. R & R LONGERON IAW DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

WING TO BODY SUPPORT CORRODED BETWEEN BS 832 TO 813, BL 0. R & R SUPPORT IAW DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

AFT CARGO COMPARTMENT FRAME CORRODED AT BS 927, LONGERON 28R - 29L. REPAIRED FRAME IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

AFT CARGO COMPARTMENT SHEAR TIE CORRODED AT BS 954, BETWEEN LONGERON 30 TO 29L. R & R SHEAR TIE IAW SRM.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

WING TO BODY SUPPORT FITTING CRACKED AT BS 835, BL 0. R & R FITTING IAW SRM & DWG.

Part: PAN — CORRODED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

DOOR CUT OUT LOWER DOOR JAMB PAN CORRODED. REPAIRED JAMB PAN IAW SRM.

Part: ANGLE — CRACKED (LE SLAT) · airframe 42,611 hrs · 29,026 cycles

LEFT WING NR 5 LE SLAT TRACK ANGLE CRACKED. R & R ANGLE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

SHEAR TIE CORRODED AT BS 974, BETWEEN LONGERON 30 - 29. REPAIRED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

SHEAR TIE CORRODED AT BS 1002, BETWEEN LONGERON 30L TO 29L. R & R SHEAR TIE IAW DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

MAIN CABIN FLOOR SUPPORT CORRODED AT BS 240, BETWEEN LBL 15 TO RBL 15. R & R SUPPORT IAW DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

MAIN CABIN SEAT TRACK CORRODED BETWEEN BS 823 TO 898.5, RBL 44. R & R SEAT TRACK IAW DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

MAIN CABIN FLOOR SUPPORT CORRODED AT BS 200, BETWEEN RBL 10 TO 44. R & R SUPPORT IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

MAIN CABIN SEAT TRACK CORRODED BETWEEN BS 823 TO 898, LBL 44. R & R SEAT TRACK IAW DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

MAIN CABIN SEAT TRACK CORRODED BETWEEN BS 645 TO 823, LBL 22. R & R SEAT TRACK IAW DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

MAIN CABIN SEAT TRACK CORRODED BETWEEN BS 645 TO 823, RBL 44. R & R SEAT TRACK IAW DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

MAIN CABIN SEAT TRACK FLANGE CORRODED BETWEEN BS 200 TO 588, RBL 44. R & R SEAT TRACK IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

MAIN CABIN SEAT TRACK CORRODED BETWEEN BS 645 TO 823, LBL 44. R & R SEAT TRACK IAW DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

MAIN CABIN FLOOR SUPPORT CORRODED BETWEEN BS 200 TO 147, RBL 7. R & R SUPPORT IAW DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

MAIN CABIN SEAT TRACK CORRODED BETWEEN BS 588 TO 645, RBL 22. R & R SEAT TRACK IAW DWG.

Part: TIE DOWN — CORRODED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

MAIN CABIN TIE DOWN CORRODED AT BS 210, RBL 10. R & R TIE DOWN IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

MAIN CABIN SEAT TRACK CORRODED BETWEEN BS 898 - 1022, LBL 44. R & R SEAT TRACK IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

MAIN CABIN FLOOR SUPPORT CORRODED AT BS 180, BETWEEN RBL 10 TO 44. R & R SUPPORT IAW DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

MAIN CABIN SEAT TRACK CORRODED BETWEEN BS 588 TO 645, RBL 44. R & R SEAT TRACK IAW DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

MAIN CABIN FLOOR SUPPORT CORRODED AT BS 180, RBL 44. R & R SUPPORT IAW DWG.

Part: CHANNEL — CRACKED (RT MLG WW) · airframe 42,611 hrs · 29,026 cycles

RIGHT WW DOOR UPPER FWD CORNER CHANNEL CRACKED. R & R CHANNEL IAW DWG.

Part: DOOR FRAME — CRACKED (L1 DOOR) · airframe 42,611 hrs · 29,026 cycles

L1 DOOR UPPER FRAME CRACKED BETWEEN BS 161.375 TO 197.375 AT AFT SIDE. REPAIRED FRAME IAW SRM & DWG.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

C1 DOOR PAN FWD & AFT REPAIR SPLICE CORRODED. R & R SPLICE IAW SRM.

Part: PAN — CORRODED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

C1 DOOR JAMB PAN LOWER SECTION CORRODED. R & R PAN IAW SRM.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 42,611 hrs · 29,026 cycles

RIGHT WING WHERE INBD BUTTE DOOR ATTACHED SUPPORT ANGLE CRACKED. R & R ANGLE IAW DWG.

Part: ANGLE — CRACKED (LE SLAT) · airframe 42,611 hrs · 29,026 cycles

RIGHT WING INBD SIDE OF NR 12 SLAT TRACK ANGLE CRACKED ON SLAT SIDE. R & R ANGLE IAW DWG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

LEFT CUSP WEB CORRODED AT STATION 794 - 813. REPAIRED WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

RIGHT CUSP WEB CORRODED AT STATION 550. REPAIRED WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

CUSP WEB CORRODED AT BS 923, RBL 59. R & R CUSP WEB IAW SRM & DWG.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

CUSP WEB CRACKED AT BS 655, RBL 59. REPAIRED CUSP WEB IAW SRM & DWG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

LEFT CUSP WEB CORRODED AT STATION 636 - 660. REPAIRED WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

LEFT CUSP WEB CORRODED AT STATION 636 - 655. REPAIRED WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

RIGHT CUSP WEB CORRODED AT STATION 598 - 617. REPAIRED WEB IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

CUSP WEB CRACKED AT BS 696, LBL 59. REPAIRED CUSP WEB IAW EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

MAIN FRAME WING TO FUSE FITTING CRACKED AT BS 661, LONGERON 22R. R & R FITTING IAW DWG.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

RIGHT CUSP WEB CRACKED AT STATION 598. REPAIRED WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

LEFT CUSP WEB CORRODED AT STATION 246. REPAIRED WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

LEFT CUSP WEB CORRODED AT STATION 488, LBL 60. REPAIRED WEB IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

SKIN SPLICE ANGLE CORRODED BETWEEN BS 636 TO 655, LBL 59. R & R ANGLE IAW EA.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

RIGHT CUSP WEB CORRODED AT STATION 740. REPAIRED WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

LEFT CUSP WEB CORRODED AT STATION 579 - 598. REPAIRED WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 42,611 hrs · 29,026 cycles

CUSP WEB CORRODED BETWEEN BS 440 TO 449, RBL 59. REPAIRED MEMBRANE IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,066 hrs · 28,662 cycles

FLOOR SUPPORT CORRODED BETWEEN BS 150 TO BS 160, LBL 12. REPAIRED SUPPORT IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,066 hrs · 28,662 cycles

MAIN CABIN FLOOR SUPPORT CORRODED AT BS 180, LBL 20. R & R SUPPORT IAW SRM & DWG.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 42,066 hrs · 28,662 cycles

COCKPIT SUB FLOOR CORRODED BETWEEN BS 133 TO BS 148, BETWEEN BL 0 TO LBL 22.5 AT EPC. REPAIRED DOUBLER IAW EA & DWG.

Part: COVER — LOOSE (EXIT SIGN) · airframe 42,053 hrs · 28,652 cycles

AFT OVERHEAD EMERGENCY EXIT ROW SIGN COVER LOOSE. SECURED SIGN IAW AMM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 40,518 hrs · 27,684 cycles

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

Part: PIN — MISSING (EVAC SLIDE) · airframe 40,144 hrs · 27,444 cycles

L1 DOOR EMERGENCY EVAC SLIDE RETAINING PIN MISSING. REINSTALLED PINS IAW AMM.

Part: LATCH — LOOSE (R1 DOOR) · airframe 39,840 hrs · 27,260 cycles

R1 DOOR EMERGENCY EVAC SLIDE LATCH LOOSE. SECURED LATCH IAW M/M.

Part: SEAL — CRACKED (LT AILERON) · airframe 37,442 hrs · 25,744 cycles

LEFT WING FIXED T/E PANELS I/B OF AILERON T/E SEAL HAS PIECES MISSING AND CRACKED. REMOVED AND REPLACED T/E PANEL T/E SEAL P/N 14D0014 PO 79019347 IAW B717 SRM 51-41-02.

Part: LENS — MISSING (CATWALK) · airframe 37,442 hrs · 25,744 cycles

LENSE COVER FOR LIGHT ASSEMBLY ON AFT ACCESSORY COMPARTEMNT CAT WALK MISSING ON CENTER LIGHT. REMOVED AND REPLACED LENSE BOXER ON AFT ACCESORY COMPARTMENT CATWALK CENTER EMERGENCY EXIT VERTICAL LIGHT IAW B717 AMM 33-51-14.

Part: VALVE — FAULTY (MLG WW) · airframe 37,442 hrs · 25,744 cycles

SELECTED LANDING GEAR DOWN, GOT 3 GEAR UNSAFE LIGHTS (RED) FOR 30 SECONDS. THEN CYCLED GEAR SECOND TRY GOT UNSAFE FOR 15 SECONDS FOR NOSE GEAR AND 20 SECONDS FOR MAIN GEAR TO 3 GREEN AND GEAR SAFE. REMOVED AND REPLACED LANDING GEAR CENTRAL VALVE IAW AMM.

Part: CONTROL VALVE — FAULTY (MLG WW) · airframe 38,084 hrs · 26,163 cycles

SELECTED LANDING GEAR DOWN AND GOT 3 GEAR UNSAFE LIGHTS (RED) FOR 30 SECONDS, THEN CYCLED GEAR. SECOND TRY GOT UNSAFE FOR 15 SECONDS FOR NOSE GEAR AND 20 SECONDS FOR MAIN GEAR. TO 3 GREEN AND GEAR SAFE. REMOVED AND REPLACED LANDING GEAR CONTROL VALVE PER MM.

Part: COVER — MISSING (CABIN) · airframe 38,011 hrs · 26,117 cycles

FORWARD OVERHEAD CABIN EMERGENCY EXIT SIGN COVER MISSING. INSTALLED COVER PER M/M.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,899 hrs · 26,047 cycles

EMERGENCY EXIT LIGHTS INOP. REPAIRED LIGHT PER AMM.

Part: COVER — MISSING (EXIT SIGN)

EMERGENCY EXIT SIGN FOR AISLE OVERHD PLASTIC COVER MISSING. INSTALLED EMER EXIT COVER.

Part: LIGHT — INOPERATIVE (CABIN)

ONE EMERGENCY ESCAPE PATH LIGHT OUT AT SEAT 2B. RELAMPED TRACK LIGHT AT SEAT 2B, OPS CHECK OK REF MM 33-50.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

AFT CARGO FWD BULKHEAD FLOOR SUPPORT, STA 813, CRACKED. ACCOMPLISHED FLOOR SUPPORT ANGLE AND FILLER REPAIR PER B717 SRM 51-41-02.

Part: SHEAR TIE — CORRODED (FUSELAGE)

AFT CARGO COMPARTMENT FUSELAGE SHEAR-TIE, STA 927, LONG L29L TO L29R, CORROSION. ACCOMPLISHED FUSELAGE SHEAR-TIE REPLACEMENT PER B717 53-00-06 AND B717 SRM 51-41-02/05.

Part: PAN — CORRODED (FUSELAGE)

AFT CARGO DOOR JAMB PAN, CORROSION. ACCOMPLISHED JAMB PAN SPLICE REPAIR PER B717 SRM 53-20-15 FIG 201 REPAIR 7.

Part: LIGHT — INOPERATIVE (CABIN)

R1 DOOR EMERGENCY EXIT LIGHT HAS ONE EACH LIGHT INOPERATIVE (ASSEMBLY WITH 5 LAMPS). REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT R1 DOOR REF B717 AMM 33-51. OPERATIONALLY CHECKS GOOD.

Part: STRUCTURE — CRACKED (FUSELAGE)

RT VENT BOX AT STA 1212 CRACKED. REPAIRED PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (BS 195-200)

FLOOR SUPPORT HAS CORROSION AT BS 195 - 200 LBL 15 OUT OF LIMITS. REMOVED AND REPLACED FLOOR SUPPORT AT BS 195 - 200 LBL 15 IAW B717 SRM 51-41-01.

Part: FLOORBEAM — CORRODED (BS 200)

FLOOR SUPPORT HAS CORROSION AT BS 200 BL-0 RBL 37. REMOVED AND REPLACED FLOOR SUPPORT AT BS 200 - BL-0 TO RBL 37 IAW B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (BS 160-258)

FWD CABIN FLOOR SUPPORT ANGLE IS CORRODED AT RBL 7 BS 160 TO BS 258. REPLACED FLOOR SUPPORT FROM BS 160 TO BS 258 LBL 7 IAW B717 SRM 51-41-01.

Part: FLOOR SUPPORT — CORRODED (BS 157-196)

FLOOR SUPPORT HAS CORROSION AT BS 157 - BS 196 RBL 36 OUT OF LIMITS. REMOVED AND REPLACED FLOOR SUPPORT AT BS 157 - BS 196 RBL 36 IAW B717 SRM 51-41-02.

Part: FLOORBEAM — CORRODED (BS 200)

FLOOR SUPPORT HAS CORROSION AT BS 200 & LBL 24 - 60 OUT OF LIMITS. REMOVED AND REPLACED FLOOR SUPPORT AT BS 200 & LBL 24 - 60 IAW B717 SRM 51-41-05.

Part: WEB — CORRODED (BS 200)

FLOOR WEB HAS CRACKS & CORROSION AT BS 200 RBL 22 CORROSION OUT OF LIMITS. FABRICATED WEB REPAIR PER B717 SRM 51-70-10.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FWD GALLEY FLOOR HAS CORRODED ANGLE BETWEEN PANELS 221 BF & 221 CF. CORROSION OUT OF LIMITS. INSTALLED NEW FLOOR SUPPORT ANGLE PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (BS 157-190)

FLOOR SUPPORT HAS CORROSION BS 157-190 RBL 46 OUT OF LIMITS. REPLACED FLOOR SUPPORT AT BS 157 - BS 190 AT RBL 46 PER B717 SRM 51-10-04.

Part: SILL — CORRODED (FUSELAGE)

R-1 DOOR SILL WEB HAS CORROSION BEYOND LIMITS. REPLACED CLOSURE RIB IAW B717 SRM 51-41-01.

Part: FLOORBEAM — CORRODED (BS 200)

FLOOR SUPPORT HAS CORROSION AT BS 200 LBL 22 OUT OF LIMITS. REMOVED AND REPLACED SUPPORT AT BS 200 LBL 22 IAW SRM 51-41-01.

Part: FLOOR SUPPORT — CORRODED (BS 160-258)

FWD CABIN FLOOR SUPPORT CORRODED AT LBL 14 FROM BODY STA 160 TO BS 258 - OUT OF LIMITS. REPLACED FLOOR SUPPORT FROM BS 160 - 258 - LBL 14 PER B717 SRM 51-41-01.

Part: FLOORBEAM — CORRODED (BS 200)

FLOOR SUPPORT HAS CORROSION AT STA 200 RBL 48-57 - OUT OF LIMITS. REPLACED FLOOR SUPPORT RBL 48 TO RBL 57 AT STA BS 200 PER B717 SRM 51-10-04.

Part: WEB — CORRODED (BS 200)

FLOOR WEB HAS CORROSION AT BL 0 - LBL 7 AT STA 200 OUT OF LIMITS. CUT OUT AFFECTED AREA, FABRICATED DOUBLER REPAIR, INSTALLED SAME PER B717 SRM 51-71-10.

Part: FLOOR SUPPORT — CORRODED (BS 200-256)

FLOOR SUPPORT HAS CORROSION AT STA 200-256 LBL 15 - OUT OF LIMITS. REPLACED FLOOR SUPPORT AT STA 200-256 LBL 15 IAW B717 SRM 51-41-02 & -05.

Part: STIFFENER — CRACKED (FUSELAGE)

VERTICAL STIFFENER CRACKED 21" LBL 21 AND NR 5 O/B AT STA 218. INSTALLED FORMED CHANNEL REPAIR ON VERTICAL STIFFENER AT LBL 21" AND NR 5 FROM O/B AT STA 218 IAW B717 SRM 51-70-11 FIG 201. MATERIAL USED 7075-0 .063, HEAT TREATED TO 7075.T6 PER B717 SRM 51-32-01, FILLER 8" X 1" X 1" X 2.5", ANGLE 19" X 2" EACH.

Part: BULKHEAD — CRACKED (FUSELAGE)

FWD BULKHEAD WEB CRACKED ON STA 218 LBL 20". INSTALLED WEB SPLICE REPAIR AT FWD BULKHEAD STA 218 LBL 20" IAW B717 SRM 51-70-10. MATERIAL USED FOR FILLER AND DOULBER 7075T6.040 AND 7075T6.050, SIZE 15.5 X 9.75 AND 11.5 X 7.75.

Part: SUPPORT — CRACKED (FUSELAGE)

HORIZONTAL GILL LINER SUPPORT CRACKED LBL 20", 2ND FROM BOTTOM AT STA 218. REPAIRED PER B717 SRM 51-70-11.

Part: SEAT TRACK — CORRODED (COCKPIT)

FIRST OFFICER'S AFT I/B SEAT TRACK CORRODED BEYOND LIMITS. REPLACED SEAT TRACK.

Part: HYDRAULIC LINE — LEAKING (NR 2 PYLON)

A -R HYD QTY LO ALERT WITH LOSS OF HYD FLUID FOLLOWED BY R ENG DRIVEN PUMP FAILURE. FOLLOWED QRH PROCEDURES. DECLARED EMERGENCY. FOUND HYDRAULIC PRESSURE LINE IN NR 2 ENGINE PYLON LEAKING. REMOVED AND REPLACED HYDRAULIC LINE, LEAK CHECK GOOD. SERVICED HYDRAULIC SYSTEM AND REPLACED MAIN GEAR DOOR SKID PADS, A/C RETURNED TO SERVICE.

Part: ODOR — DETECTED (TRASH CAN)

A/C DIVERTED DUE TO POSSIBLE BURNING ODOR COMING FROM GALLEY / R-1 DOOR AREA. INSPECTED AIRCRAFT AND FOUND ODOR COMING FROM GALLEY TRASH CAN. RAN AIRCRAFT AND NO ODORS NOTED. ALL SYSTEMS CHECK GOOD. TRASH CAN BAGGED AND PLACED IN FORWARD CARGO COMPARTMENT.

Part: CHECK VALVE — MALFUNCTIONED (CABIN AIR)

RIGHT PAC FLO DISAGREE, AMBER PACK ALERT. AFT CABIN TEMP GOT HOT, ESPECIALLY IN AFT LAV, PACK SHUT DOWN. TEMP COOLED, INSULATION BLOWN AROUND BACK OF AIRCRAFT. REMOVED AND REPLACED COND AIR CHECK VALVE ASSY, OPS LEAK CHECK GOOD. REF TO 21-22.

Part: FRAME — DAMAGED (FUSELAGE)

RIGHT HAND FUSELAGE FRAME DAMAGED AT STA 58.750. REPLACED FUSELAGE FRAME AT STA 58.75 PER DWG 9911502 AND B717 SRM 51-41-01 (RT SIDE).

Part: FRAME — DAMAGED (FUESLAGE)

RIGHT HAND FUSELAGE FRAME DAMAGED AT STA 47.875. REPLACED FUSELAGE FRAME AT STA 47.87 PER DWG 9911501 AND B717 SRM 51-41-01 (RT SIDE).

Part: ATTACH FITTING — CRACKED (FUSELAGE)

T-CLIP CRACKED AT STA 58-750 FRP. REPLACED T-CLIP AT STA 58.75 PER DWG 9911502 AND B717 SRM 51-41-01. MATERIAL USED 7075-0, 2 X 3 INCHES LONG. HEAT TREATED TO 7075-T6 AS PER 98 PMS 247 PS-01.

Part: SKIN — DAMAGED (FUSELAGE)

RIGHT HAND FUSELAGE SKIN DAMAGED STA 37 TO STA 110. INSTALLED NEW SKIN PANEL FROM STA 37 TO STA 110, BETWEEN L18R AND L27R AS PER DWG 5911400 AND B717 SRM 51-40-2.

Part: RELAY — FAILED (ELECTRICAL SYS)

EMERGENCY POWER RELAY STUCK CLOSED. CYCLING SWITCH HAD NO EFFECT. A/C WAS DRAINING BATTERIES. MAINTENANCE REMOVED AND REPLACED A/C BATTERIES AS A PRECAUTIONARY. REMOVED AND REPLACED LEFT DCDU, LBTR, LEPR.

Part: GASPER FAN — INOPERATIVE (ACM BAY)

AFTER TAKEOFF WITH LEFT PACK OFF, NOXIOUS ODOR SMELLED HEAVILY. TURNED LT BLEED OFF, ODOR SUBSIDED. FLIGHT ATTENDANT ILL, FLIGHT DIVERTED TO MCO. REPORTED MILD SMELL WHEN POWER ADVANCED FOR LANDING. FOUND GASPER FAN MAKING A LOT OF NOISE, CAUSING BAD ODOR. REMOVED AND REPLACED GASPER FAN IAW 21-23.