N997AT

Part: OIL SYSTEM — LEAKING (APU) · airframe 60,321 hrs · 43,044 cycles

SHIP 9545 MUSTY SOCK SMELL FROM FORWARD GALLEY VENT. FOUND APU OIL LEAKING. R/R APU PER B717 AMM 49-10 OPS CHK GOOD (7952228)

Part: SIGN — DISLODGED (ZONE 200) · airframe 60,276 hrs · 42,999 cycles

FWD EXIT SIGN DAMAGED. (F/A REPORTED PASSENGER HIT IT WITH HIS BAG). RESECURED, OPS NORMAL. (LP 7952210)

Part: WARNING MESSAGE — FALSE ACTIVATION (STAB TRIM) · airframe 60,099 hrs · 42,843 cycles

ATO- DURING TAKEOFF ROLL THE CREW REPORTED A STAB OUT OF TRIM AURAL WARNING AND ABORTED TAKEOFF. MAINTENANCE PERFORMED STABILIZER SYSTEM TESTS AND RETURNED TO SERVICE.(7843690)

Part: FASTENER — LOOSE (ZONE 300) · airframe 57,977 hrs · 40,954 cycles

-AD- FOUND LOOSE FASTENERS ON LH VERTICAL STABILIZER LEADING EDGE REF AA 553001048 AND AD 2018-10-08. SUMMARY OF NRC 018-0001:5530-01048-02 /001 00004: CHECKED AND FOUND OK. SUMMARY OF NRC 018-0001:5530-01048-02/001 00004: CMOR VERIFIED LH FASTENER HOLES LIMITS IAW SG95550001 AS PER AD 2018-10-08. (LP #0675274)

Part: FASTENER — LOOSE (ZONE 300) · airframe 57,983 hrs · 40,959 cycles

-AD- FOUND LOOSE FASTENERS ON RH VERTICAL STABILIZER LEADING EDGE REF AA 553001048 AND AD 2018-10-08. SUMMARY NRC 018-0001:5530-01048-02 / 002 00005: CHECK IF THE FASTENER(S) HOLE COUNTER SINK AND DIAMETER ARE WITHIN LIMITS LISTED IN SERVICE GENERAL DRAWING SG95550001 PER AA 5530-01048 LOG-PAGE UPDATED @ 24NOV24 1450 UTC ALTD BY CHRISTENSEN 00034311 ATG 25NOV24 ENTR 00034311 F SUMMARY SEE NR FOR ADDITIONAL INFORMATION 018-0001:5530-01048-02/002 00005 CHECKED -IF- THE FASTENER HOLE COUNTER SINK AND DIAMETER ARE WITHIN LIMITS LISTED IN SERVICE GENERAL DRAWING SG95550001 PER AA 5530-01048. WAITING ON DETERMINATION, SUPPLEMENTAL TO FOLLOW. (LP #0675998)

Part: SKIN — BENT (FUSELAGE) · airframe 56,120 hrs · 39,352 cycles

BENT ON EDGE EXTERNAL SKIN AFT UPPER, AFT LOWER, AND BEAM #4 AT SERVICE DOOR L1. SUMMARY OF NRC 00069: EXTERNAL SKIN ON AFT UPPER EDGE AND EDGE OF EXTERNAL SKIN AT BEAM #4 WAS CONFORMED PER B717 SRM-51-20-09-0G. AFT LOWER EDGE OF EXTERNAL SKIN AT SERVICE DOOR L1 WAS REPAIRED PER B717-200 SRM 52-10-01-2R PROCEDURE 1, REPAIR 1, PAR 4, B, FIGURE 201. (LP #0189245)

Part: WEB — CRACKED (BS 715) · airframe 56,120 hrs · 39,352 cycles

CRACK MEMBRANE ON UPPER SURFACE OF CENTER WING STA Y=715 AND -X=44 UNDER RH MIDDLE SEAT TRACK AT WING BOX AREA. SUMMARY OF NRC 00357: MEMBRANE ON UPPER SURFACE OF CENTER WING STA Y=715 AND -X=44 UNDER RH MIDDLE SEAT TRACK AT WING BOX AREA WAS REPAIRED PER PRI 615114-14 REV 3 AND ERA 615114-14 REV ORIGINAL, SECTION I: PERMANENT REPAIR. ASSOCIATED ERA 14-615114 ADDED FOR AC 9545. (LP #0184517)

Part: DOOR FRAME — CORRODED (BS 951-994) · corrosion level 2 · airframe 56,120 hrs · 39,352 cycles

CORROSION ON DOOR JAMB STA 951 TO STA 994 AT AFT CARGO COMPARTMENT. C2. SUMMARY OF NRC 00071: CORROSION LEVEL 2. PREVIOUS REPAIR SECTION OF DOOR JAMB STA 951 TO STA 994 AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 53-20-15-2R PROCEDURE 7 REPAIR 7. (LP #0181724)

Part: SKIN — CORRODED (BS 655-663) · corrosion level 2 · airframe 56,120 hrs · 39,352 cycles

CORROSION ON INNER SKIN BTW STA Y=655/663 AND BTW LONGERONS 29L/29R AT FWD CARGO COMPARTMENT (C1). SUMMARY OF NRC 00166: CORROSION LEVEL 2. INTERNAL SKIN DOUBLER BTW STA Y=655/663 AND BTW LONGERONS 29L/29R AT FWD CARGO COMPARTMENT WAS REPAIRED PER ERA 614961-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 614961-14 REV 1. ACCOMPLISH REPETITIVE INSPECTIONS WITHIN EVERY 8,000 FLIGHT CYCLES AFTER ACCOMPLISHMENT OF SECTION I REPAIR, LOG 0178932 PER E/RA 614961-14 REV ORIGINAL, SECTION II. ASSOCIATED ER/A 14-614961 ADDED FOR AC 9545. (LP #0182991)

Part: LONGERON — CORRODED (BS 360 L26R) · corrosion level 2 · airframe 56,120 hrs · 39,352 cycles

CORROSION ON LOWER SURFACE LONGERON END STA 360 L26R AT FWD COMPARTMENT (C1). SUMMARY OF NRC 00172: CORROSION LEVEL 2. CLIP LONGERON END STA 360 L26R AT FWD COMPARTMENT (C1) WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #0181288)

Part: FLOOR SUPPORT — CRACKED (BS 655) · airframe 56,120 hrs · 39,352 cycles

CRACK ON FLOOR CHANNEL STA 655 X=-42 Z=-1 APPROX AT FWD COMPARTMENT (C1). SUMMARY OF NRC 00170: FLOOR CHANNEL STA 655 X=-42 Z=-1 APPROX AT FWD COMPARTMENT (C1) WAS REPAIRED PER B717-200 SRM 51-70-11- 2R PROCEDURE 1 REPAIR 1 PARAGRAPH 4 FIGURE 201. (LP #0171182)

Part: CUSP WEB — CORRODED (BS 160-200) · corrosion level 2 · airframe 56,120 hrs · 39,352 cycles

CORROSION ON ANGLE CUSP BTW STA Y=168 AND STA Y=200, AND STA X=-60 AT PASSENGER COMPARTMENT (R1 ENTRY). SUMMARY OF NRC 00245: CORROSION LEVEL 2. CUSP ANGLE BTW STA Y=168 AND STA Y=200, AND X=-60 AT PASSENGER COMPARTMENT (R1 ENTRY) WAS REPAIRED PER ERA 614741-14 REV ORIGINAL, SECTION I: PERMANENT REPAIR AND PRI 614741-14 REV 3. ASSOCIATED ERA 14-614741 ADDED FOR AC 9545. (LP #0170512)

Part: ANGLE — CRACKED (BS 186) · airframe 56,120 hrs · 39,352 cycles

CRACK ON ANGLE STA Y=186 AND BTW BEAMS #4/5 AT SERVICE DOOR L1. SUMMARY OF NRC 00073: ANGLE (INTERCOSTAL) STA Y=186 AND BTW BEAMS #4/5 AT SERVICE DOOR L1 WAS MANUFACTURED AND REPLACED PER DWG 9955763 REV K, B717-200 SRM 51-41-02-0G, AND 51-41-05-0G. (LP #0164029)

Part: WEB — CRACKED (BS 715) · airframe 56,120 hrs · 39,352 cycles

CARCK ON WEB STA Y=715 -X=44 CABIN FLOOR AT CPAX. SUMMARY OF NRC 00342: WEB STA Y=715 -X=44 CABIN FLOOR AT CPAX WAS REPAIRED PER B717 SRM 53-00-55-2R-4. (LP #0161024)

Part: CUSP WEB — CORRODED (BS 435-465) · corrosion level 2 · airframe 56,120 hrs · 39,352 cycles

CORROSION ON RH CUSP WEB LOWER SURFACE BTW STA Y=435 TO Y=465 PAX CABIN. SUMMARY OF NRC 00558: CORROSION LEVEL 2. RH CUSP WEB BTW STA Y=435 TO Y=465 PAX CABIN WAS REPAIRED PER B717 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #0159555)

Part: WEB — CRACKED (UNKNOWN) · airframe 56,120 hrs · 39,352 cycles

CRACKS ON WEB BTW STA Y=693 TO Y=615, -X=57, CABIN FLOOR AT CPAX. SUMMARY OF NRC 00346: WEB BTW STA Y=693 TO Y=615, -X=57, CABIN FLOOR AT CPAX WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 FIG 203. (LP #0156605)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 56,120 hrs · 39,352 cycles

CORROSION ON RH CUSP WEBS STA 870 TO 889, L-18R CABIN FLOOR AT CPAX. SUMMARY OF NRC 00485: CORROSION LEVEL 2. CUSP WEBS STA 870 TO 889, L-18R CABIN FLOOR WERE REPAIRED PER B717-200 SRM 53-00-55-2R-4. (LP #0153367)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 56,120 hrs · 39,352 cycles

CORROSION ON MEMBRANE WEB AT STA Y=198 AND STA X=-56 AT PASSENGER COMPARTMENT (W1). SUMMARY OF NRC 00247: CORROSION LEVEL 2. MEMBRANE WEB AT STA Y=198 AND STA X=-56 AT PASSENGER COMPARTMENT (W1) WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 2 REPAIR 2 PAR 4 A. (LP #0150312)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 56,120 hrs · 39,352 cycles

CORROSION OF MEMBRANE WEP ON STA Y=198 AND STA X=-56 AT PASSENGER COMPARTMENT (W1). SUMMARY OF NRC 00247: CORROSION LEVEL 2. MEMBRANE WEP ON STA Y=198 AND STA X=-56 AT PASSENGER COMPARTMENT WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 2 REPAIR 2 PAR 4 A. (LP #0150367)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,120 hrs · 39,352 cycles

CRACKED WEB AT STA Y=674 -X=44 CABIN FLOOR IN CPAX. SUMMARY OF NRC 00336: CRACK ON WEB STA Y=674 -X=44 CABIN FLOOR IN CPAX WAS REPAIRED PER B717 SRM 53-00-55-2R-4. (LP #0147690)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,048 hrs · 39,299 cycles

DENT ON 1L DOOR SKIN. LEFT LOWER CORNER. DENT MEASURES 3" X .5". FOUND DAMAGE TO PRESSURE SEAL MEASURES APPROX 1.5'. ACCOMPLISHED SECTION 1 FERRY FLIGHT PREPERATION IAW ERA 614189-14 REVISION ORIGINAL. CUT OUT DAMAGE AND REMOVED EXISTING FASTNER FOR REPAIR PER B717 SRM 52-10-01-2R-1 PROCEDURE 1. ACCOMPLISHED DAMAGE CONTAINMENT EDDY CURRENT INSPECTION PER DC NTM/SPM 06-10-01.001. NO CRACKS NOTED . DELTA QC 5289 329603 FABBED, TREATED, AND PRIMED REPAIR PER B717 SRM 52-10-01-2R-1. INSTALLED REPAIR PER B717 SRM 52-10-01-2R-1. RII COMPLETE DELTA QC 5399 554090 TOP COATED, PERMENANT REPAIR, JOB COMPLETE. PRESSURE SEAL ON N/R CARD. (LP #4289674)

Part: BATTERY PACK — INOPERATIVE · airframe 52,560 hrs · 36,163 cycles

FOUND THE CENTER OVERWING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE CENTER OVERWING EMERGENCY LIGHT BATTERY PACK REF B717 AMM 33 -51. OPERATIONAL CHECK WAS NORMAL. (LP #8632816)

Part: GASPER FAN — SEIZED · airframe 52,501 hrs · 36,101 cycles

SHIP 9545 - THE FLIGHT CREW DIVERTED THE AIRCRAFT TO JAX DUE TO A STRONG ODOR IN THE COCKPIT AND SMOKE IN THE CABIN AS REPORTED BY THE CABIN CREW. AN EMERGENCY WAS DECLARED WITH ATC AND THE LANDING AT JAX WAS UNEVENTFUL. CORRECTIVE ACTION: MAINTENANCE FOUND THAT THE GASPER FAN HAD SEIZED AND THEN SMOKED. THE FAN AND COALESCER BAGS WERE ALL REPLACED. OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT RETURNED TO SERVICE. (LP #8616278)

Part: NONE — NONE · corrosion level 2 · airframe 51,718 hrs · 35,397 cycles

AFT CARGO LOWER DOOR JAMB FROM MID DOOR TO FWD END OF JAMB HAS LARGE AREAS OF SURFACE CORROSION.(M) SUMMARY SEE NRC 054-0009 5300-2007/002 00319: CORROSION LEVEL 2. BLENDED OUT CORROSION AND CHECK LIMITS PER B717 SRM 53-00-00-01A. NDT REQUIRED. PERFORMED U/T OF MATERIAL REMAINING THICKNESS IAW BOEING 717 NDT SPM PART 04-10-01.002 FOUND TO BE OUT OF LIMITS IAW B717 SRM 53-00-00-01A. REMOVED 2EA SPLICES, 1 FITTING, LOWER SCUFF PLATE, AND LOWER JAMB PAN FROM AFT CARGO DOOR JAMB PER B717 SRM 51-41-02 AND B717 SRM 51-41-01. LOCATED, DRILLED, AND INSTALLED NEW WEB PAN PER B717 SRM 51-40-08 & 53-00-00-01A. INSTALLED 2EA SPLICES, 1 FITTING, AND LOWER SCUFF PLATE IAW B717 SRM 51-40-02. (LP #2047195)

Part: NONE — NONE · airframe 51,597 hrs · 35,290 cycles

THE EMERGENCY FLOOR PATH LIGHTING AT 19D IS MISSSING. MAINTENANCE REPLACED 19D EMERGENCY FLOOR LIGHT STRIP PER B717 AMM 33-50. OPERATIONAL CHECK WAS GOOD. (LP #2004641)

Part: NONE — NONE · airframe 51,389 hrs · 35,106 cycles

THE FORWARD ATTENDANT EMERGENCY EXIT SIGN AND THE CEILING PANELS #11 AND #12 EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENACE REPLACED THE EMERGENCY BATTERY PACKS AT LOCATIONS B5-235 AND B5- 231 PER B717 AMM 33-51. OPERATIONAL CHECK IS NORMAL. (LP #8080547)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 51,185 hrs · 34,915 cycles

THE RIGHT AND LEFT AFT OVERWING EXIT LOWER EMERGENCY EXIT LIGHTS ARE INOPERATIVE. IN REFERENCE TO THE B717 AMM 33-51, MAINTENANCE REPLACED THE EXIT LIGHT POWER AND BATTERY. THE OPERATIONAL TEST WAS GOOD. (LP #7807637)

Part: NONE — NONE · airframe 51,718 hrs · 35,397 cycles

LEADING EDGE SLAT TRACK CUTOUT MISSING ON #3 SLAT. FORWARD CUTOUT DOOR TO CDL 57-47-01. PLACARD INSTALLED. MISSING PART NUMBER IN IPC IS NOT EFFECTIVE FOR THIS A/C. PER BOEING CUSTOMER SUPPORT THERE IS AN IPC MISPRINT WHICH WILL BE CORRECTED IN JANUARY OF 2022. MAINTENANCE IS IN PROGRESS... (LP #7296660)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 50,439 hrs · 34,308 cycles

THE EMERGENCY EXIT IDENTIFIER LIGHT AT THE FIRST ROW OF SEATS AND THE OVERHEAD EMERGENCY FLOODLIGHT AT THE SERVICE DOOR ARE BOTH INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK BP-259 PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #7296636)

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 49,704 hrs · 33,730 cycles

VERTICAL STAB ZFS 52.267 LT SKIN CRACK INDICATION. MAINTENANCE COMPLIED WITH ALL STEPS OF PRI 588955-14AD REV ORIG, 1, 2, 3, AND 4. COMPLIED WITH TIME LIMITED REPAIR SECTION 1 OR ER/A 588955-14AD REV ORIGINAL.

Part: SPAR CAP — CRACKED (VERTICAL STAB) · airframe 49,704 hrs · 33,730 cycles

THE THIRD BOLT HOLE BELOW STA ZFS=52.267 ON LT VERTICAL STAB FRONT SPAR CAP HAS CRACK INDICATION, REF AA 5530-01048 AND AD 2018-10-08. MAINTENANCE COMPLIED WITH CRACK VERIFICATION, PER AMDS 5530-01048-02 AND CRACK INDICATION STILL PRESENT. VERIFIED CRACK IN SKIN/DOUBLER NOT SPAR CHORD, PER BHEC. CRACK DETERMIND IN SKIN (QC1432). STEPPED SKIN HOLE TO .215. STEPPED HOLE TP .264. COMPLIED WITH CRACK INSPECTION BHEC OF SKIN-NO CRACK. DAMAGED HOLE REPAIRED, PER ERA/PRI 1 588955-14 REV 4. COMPLIED WITH ER/A 588955-14 AD REV ORG FINAL ER/A MATCHES PRI. ASSOCIATED ER/A 14-588955 ADDED FOR AC 9545.

Part: SPAR CAP — CRACKED (VERTICAL STAB) · airframe 49,704 hrs · 33,729 cycles

4TH BOLT HOLE BELOW STA ZFS=52.267 ON LT SIDE OF VERTICAL STAB FRONT SPAR CAP HAS CRACK INDICATION, REF AA5530-01048 & AD 2018 -10-08. C/W CRACK VERIFICATION, PER AMDS 5530-01048-02 STEP 10. CRACK DETERMINED IN SKIN (QC1432). STEPPED SKIN HOLE TO .277. C/W HFEC OF SKIN-NO CRACK (QC1432). DAMAGED HOLE REPAIRED, PER ERA/PRI 588955-14 REV 4. C/W ER/A 58895514-AD REV ORIG FINAL ER/A MATCHES PRI, ASSOCIATED AA 5530-01048 ADDED FOR AC 9545, ASSOCIATED ER/A 14-588955 ADDED FOR AC 9545.

Part: NONE — NONE · airframe 53,328 hrs · 36,894 cycles

DAMAGE TOLERANCE EVALUATION ERA 5882955-14AD ISSUED FOR VERTICAL STABILIZER SKIN CRACK REPAIR. FOLLOW ON ACTION REQUIRED. ACCOMPLISH DAMAGE TOLERANCE EVALUATION PRIOR TO 24 MONTHS FROM SECTION I ACCOMPLISHMENT. ERA REVISION REQUIRED FOR A/C OPERATION BEYOND 24 MONTHS. REFERANCE ERA 588282 AND LOG 1639967 FOR EXISTING REPAIR AND DAMAGE TOLERANCE EVALUATION. DEFER ASSOCIATED AA 5530-01048 ADDED FOR AC 9545. ASSOCIATED ER/A 00-588955 ADDED FOR AC 9545. ERA 588955-14AD REV A IS CURRENT, THIS LP MAY BE CLOSED AND REMOVE MONITOR INSP PER ALERT 28SEP22 AND LOG COMMENTS. (LP #1674753)

Part: FRAME — CRACKED (TAILCONE) · airframe 49,638 hrs · 33,674 cycles

A CRACK WAS FOUND ON THE REAR FRAME (48 SECTION UPPER). THE AFT TAIL CONE WAS DROPPED. MAINTENANCE REMOVED THE DAMAGED 48 SECTION OF THE UPPER FRAME AND INSTALLED A NEW 48 SECTION UPPER FRAME, PER BOEING DRAWING 5966768.

Part: ACCESS DOOR — MISSING (RT ELEVATOR) · airframe 49,592 hrs · 33,637 cycles

DURING THE POST-FLIGHT INSPECTION, THE PILOT DISCOVERED THAT THE RIGHT ELEVATOR OUTBOARD MOST HINGE NUT LOWER ACCESS DOOR WAS MISSING. MAINTENANCE FORWARDED IT TO CDL 55-25-01, DUE TO NOT A STOCK ITEM. NO "M" PROCEDURES. PLACARD WAS INSTALLED. ALSO, PERFORMANCE CORRECTIONS APPLIED REF IPC 55-21-01-01.

Part: SKIN — CRACKED (VERTICAL STAB LE) · airframe 49,508 hrs · 33,560 cycles

THE RT SIDE OF VERTICAL STAB LEADING EDGE HAS A CRACK INDICATION IN HOLE NR 3 BELOW STA 2FS=52.267, REF AMDS CARD 5230-01048-02 STEP 8, AA 5530-01048 AD 2018-10-08. INSPECTED RT HORIZONTAL STAB HOLE NR 3. BHEC IAW CARD 5330-01048-02. CRACK INDICATION IS IN ONLY OF HORIZONTAL STAB "OTHER SKIN ONLY". CLEANED NR 3 HOLE UP TO .270 DRILL BIT, IAW PRI ER/A 588282-14 REV ORIG PRI REV 1. PERFORMED BEHC, IAW CARD 5330-01048-02. NO CRACK INDICATION (QC 1315)881955, REF PRI ER/A 588282-14.

Part: SKIN — CRACKED (VERTICAL STAB LE) · airframe 49,508 hrs · 33,560 cycles

LT SIDE OF VERTICAL STAB LEADING EDGE HAS 3 CRACK INDICATIONS IN HOLES NR 2, 3, & 4 BELOW STA 2FS=52.267, REF AMDS CARD 5530-01048-02 STP 8, AA5530-01048 AD 2018-10-08. RE-EVALUATION OF FASTENER HOLES FOUND HOLES NR 3 & 4 WITH NO CRACK INDICATION. HOLE NR 2 STILL HAS CRACK ON OUTER SKIN ONLY, IAW CARD 5530-01048-02 REV ORIG CLEANED NR 2 HOLE UP TO (B) DRILL BIT .237, IAW ER/A 58828-14 REV ORIG PRI REV 1. ASSOCIATED AA 5530-01048 ADDED FOR AC 9545.

Part: NONE — NONE · airframe 53,328 hrs · 36,894 cycles

DAMAGE TOLERANCE EVALUATION IN REFERENCE TO ERA 588282-14AD. ASSOCIATED ER/A 14-588282 ADDED FOR AC 9545. UPDATED MONITOR TITLE. REFER TO ERA 588955-14AD AND MONITOR 1674753 FOR ADJACENT REPAIR WHICH ALSO IS PENDING STAGE II/ III DAMAGE TOLERANCE EVALUATION. NO CHANGE TO THIS LOG OR MASK. ERA 588282-14AD REV A IS NOW CURRENT. THIS LP MAY BE CLOSED AND REMOVED MONITOR INSPECTION PER ALERT 28SEP22 AND LOG COMMENTS. (LP #1639967)

Part: FRAME — CRACKED (BS 696) · airframe 46,341 hrs · 31,007 cycles

FUSELAGE FRAME AT STA Y 696 RT SIDE HAS A CRACK. REF AA 5310-01436 CRACK IS CONDITION 3. NRC 026-0004:5310-01436-01D/001 00060: REPLACED FRAME AT STA 696 RH PER WORK CARD 5310-01436-03B. (LP #1037420)

Part: SLIDE — UNSERVICEABLE (TAIL CONE) · airframe 45,334 hrs · 30,318 cycles

DURING TAIL CONE ESCAPE SLIDE PIN CHECK, MAINTENANCE FOUND THE SLIDE TO BE UNSERVICEABLE (FAULT NOT SPECIFIED). MAINTENANCE REPLACED THE TAIL CONE SLIDE PER B717 AMDS CARD 2561-9006. NO FURTHER DEFECTS NOTED. THE AIRCRAFT HAS RETURNED TO SERVICE. (LP #4427198)

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 43,288 hrs · 28,904 cycles

RIGHT EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT IAW AMM 33-50, OPS CHECKED GOOD.

Part: DOUBLER — CRACKED (BS 1178) · airframe 41,521 hrs · 27,768 cycles

CRACK ON PRODUCTION DOUBLER BS 1178 BETWEEN LONGERONS 19R TO 20R. REPAIRED IAW DWG 9911859, REV BU AND SRM 51-20-09.

Part: CARGO TRACK — CORRODED (BS 813-1028) · corrosion level 2 · airframe 41,521 hrs · 27,768 cycles

CORROSION ON LEFT CARGO TRACK FROM BS 813 TO 1028. THE CARGO TRACK WAS REPLACED IAW SRM 51-41-01 AND 51-41-02.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 41,521 hrs · 27,768 cycles

CORROSION ON AREA COUNTERSINK ON FUEL TANKS ACCESS PANEL 520CB. THE ACCESS PANEL WAS REPLACED IAW SRM 57-10-01.

Part: CHANNEL — CRACKED (LT MLG DOOR) · airframe 41,521 hrs · 27,768 cycles

CRACKED CHANNEL AFT INBD SIDE ON THE LT MLG INBD DOOR. REPAIRED IAW ER/A 558127-14, REV ORIGINAL, AND ETI-17-17-063, REV ORIGINAL.

Part: BRACE — CORRODED (NLG) · corrosion level 2 · airframe 41,521 hrs · 27,768 cycles

CORROSION ON DRAG BRACE ASSEMBLY AT NLG. THE DRAG BRACE WAS REMOVED AND REPLACED IAW AMM 32-22-05 000-801, AMM 32-22-05 400-802 AND 32-22-05 400-801.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 41,521 hrs · 27,768 cycles

CRACK ON LONG 8L AND STA Y=1022. DAMAGED LONGERON WAS REPLACED PER SRM 53-00-05-2R, 51-41-02, AND 51-41-05.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,521 hrs · 27,768 cycles

CRACK ON FRAME AT STA Y=1037 BTW LONG'S 16R AND 18R. FRAME AT STA Y=1037 BTW LONG 16R AND 18R WAS REPAIRED PER SRM 53-20-07-2R REP 4.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,521 hrs · 27,768 cycles

CRACK ON FRAME AT STA Y=1037 BTW LONG 16L AND 18L. FRAME WAS REPAIRED PER SRM 53-20-07-2R REP 4.

Part: FITTING — CRACKED (FUSELAGE) · airframe 41,521 hrs · 27,768 cycles

CRACKED FRAME CLIP BELOW LONG 16R AND STA Y=1022 (CPAX). FRAME CLIP WERE REPLACED PER DGW 9912243 REV JS AND SRM 51-41-05.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,521 hrs · 27,768 cycles

CRACKED FRAMES IN STA Y=693 AND Y=678 LT AND RT SIDE AT UNDER WING CANTED KEEL. FRAMES (4EA) WERE REPAIRED PER SRM 51-70-11 REPAIR 1.

Part: ACCESS PANEL — DAMAGED (WING) · airframe 41,521 hrs · 27,768 cycles

ELONGATE HOLES ON FUEL TANKS ACCESS PLATES 520LB, 141AL, AND 141AR. ACCESS PLATES WERE REWORKED AND FOUND 6 HOLES OUT OF LIMITS PER SRM 57-10-01-2R B CONDITION II. FABRICATED BUSHINGS PER SRM 57-10-01-2R B CONDITION II(1), (3) (D) FOR 520 LB, AND SRM 57-10-01-2R B CONDITION II (1) (2), (D) FOR 141AL AND 141AR WITH AN INTERFERENCE FIT OF 0.0005" TO 0.0015". THE BUSHINGS WERE INSTALLED ON ACCESS PLATE 141AL (4E/A), 141AR (1E/A), AND 520LB (1E/A) PER SRM 57-10-01-2R-2.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 41,521 hrs · 27,768 cycles

CORROSION ON SETTLEMENT AREA OF FUEL ACCESS 620CT AND 520CT. BLEND OUT REPAIR IS NOT PERMITTED ON THE UPPER WING ACCESS DOOR DUE TO THE REDUCED AREA OF THE CONDUCTIVE INTERFACE THEREFORE FUEL ACCESS PLATES WERE REPLACED PER SRM 57-10-01 AND PART NUMBER WAS VERIFIED PER IPC 57-22-01.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,521 hrs · 27,768 cycles

CORROSION ON RT CUSP WEB STA Y=493 IN REF NRC 00388 5300-2020. REPAIR WAS ACCOMPLISHED PER SRM 53-00-55-2R-4.

Part: BEAM — CRACKED (FUSELAGE) · airframe 41,521 hrs · 27,768 cycles

CRACK ON DOOR JAMB BEAM RT SIDE Y=41 APPROX AT NLG WHEEL WELL. DOOR JAMB BEAM RT SIDE WAS REPAIRED PER SRM 53-10-14 REPAIR 2 FIGURE 201.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 41,521 hrs · 27,768 cycles

CRACK ON RT CUSP MEMBRANE FROM STA Y=894 TO Y=896, BTW X=58-60 REF CARD 385. REPAIR WAS PERFORMED PER SRM 53-00-55-2R. HFEC INSPECTION WAS ACCOMPLISHED AFTER DAMAGE REMOVED AND NO CRACKS WERE FOUND PER NDT SPM 06-10-01.001. SPLICE WAS REMOVED AND INSTALLED PER SRM 51-41-05.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 41,521 hrs · 27,768 cycles

CRACK ON LONG 6L AND STA Y=1022. DAMAGE SECTION WAS REPLACED PER SRM 53-00-05-2R.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 41,521 hrs · 27,768 cycles

CRACK ON FLOOR PANELS 222AFF, 222ALF, 222AJF, AND 222AF. FLOOR PANELS WERE REPAIRED PER SRM 53-20-50-2R-5. HFEC INSPECTION WAS ACCOMPLISHED ON FLOOR PANELS 222AFF, 222ALF, 222AJF, AND 222AF. NO CRACKS WERE FOUND AFTER STOP DRILLING PER SRM 53-20-50-2R-5, GENERAL NOTES, STEP 25 AND NDT SPM 06-10-01.001.

Part: SKIN — DENTED (TE FLAP VANE) · airframe 41,521 hrs · 27,768 cycles

DENT ON LT WING AFT MOVABLE VANE LOWER SURFACE 8" FROM INBD AND 5" FROM T/E. DENT ON LT WING AFT MOVABLE VANE LOWER SURFACE AT 8" FROM INBD AND 5" FROM T/E WAS REPAIRED PER SRM 57-53-01-2R-1 AND OPN 1031, CARD 2000-8149-01.

Part: BEAM — CRACKED (FUSELAGE) · airframe 41,521 hrs · 27,768 cycles

CRACK ON DOOR JAMB BEAM LT SIDE Y=41 APPROX AT NLG WHEEL WELL. DOOR JAMB BEAM LT SIDE WAS REPAIRED PER SRM 53-10-14 REPAIR 2 FIGURE 201.

Part: FLOOR PANEL — DAMAGED (COCKPIT) · airframe 41,521 hrs · 27,768 cycles

DAMAGE ALL FLOOR PANELS OF COCKPIT. FLOOR PANELS OF COCKPIT DAMAGE WERE REPAIRED PER SRM 53-20-50-2R-3- AND FLOOR PANELS 211ALF AND 211ANF WERE FABRICATE PER SRM 53-20-50 2R-3.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,521 hrs · 27,768 cycles

CORROSION ON LT CUSP WEB BTW X=54-60 STA Y=541-560 UPPER AND LOWER SURFACE AT PAX CABIN IN REF 5300-2020. DAMAGE WAS REPAIRED PER SRM 53-00-55-2R.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,521 hrs · 27,768 cycles

CORROSION ON RT CUSP WEB STA Y=419 X=-56 AT PAX CABIN IN REF NRTC 00388. CUSP WEB WAS REPAIRED PER SRM 53-00-55-2R-4, 51-41-02, 51-10-04 PAR 37.

Part: CUSP WEB — CORRODED (BS 598-617) · corrosion level 2 · airframe 41,521 hrs · 27,768 cycles

CORROSION ON THE CUSP WEB BETWEEN LBL 54 - 60, BS 598 - 617 UPPER AND LOWER SURFACES. THE CUSP WEB WAS REPAIRED IAW SRM 51-41-02, 53-00-55-2R-4, AND 51-10-04, PAR 37, REPAIR 4.

Part: CUSP WEB — CRACKED (BS 223) · airframe 41,521 hrs · 27,768 cycles

CRACKED CUSP WEB, RBL 54 AND 60, BS 223. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R, FIG 215, AND 51-41-02.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 41,521 hrs · 27,768 cycles

DENT ON UPPER SURFACE (MID SECTION) AT FWD MOVABLE FLAP VANE, LH WING (SM)(AI). NR 00197 DENT ON UPPER SURFACE (MID SECTION) AT FWD MOVABLE FLAP VANE, LH WING WAS MEASURED, DENT 1 DIAMETER 1" AND DEPTH 0.034" THEREFORE IS WITHIN LIMITS PER B-717 SRM 57-53-01-1A, EQUIPMENT USED P/N: 543-402 VENCE: 17OCT17 S/N 1177, DETAIL VISUAL INSPECTION (DVI) AND TAP-TEST WAS PERFORMED, ADITIONAL DAMAGE WAS NOT FOUND PER B-717 SRM 57-53-01-1A PAR. FOR VISUAL INSPECTION SEE REFERENCE LOG 0037896 PER SRM 57-53-01-1A PAR 2.B. (LP #0037908)

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 41,521 hrs · 27,768 cycles

DENT ON UPPER SURFACE (MID SECTION) AT FWD MOVABLE FLAP VANE , LH WING (SM)(AI). NR 00197 DENT ON UPPER SURFACE (MID SECTION) AT FWD MOVABLE FLAP VANE, LH WING WAS MEASURED, DENT 1 DIAMETER 1" AND DEPTH 0.034" THEREFORE IS WITHIN LIMITS PER B-717 SRM 57-53-01-1A, EQUIPMENT USED P/N: 543-402 VENCE: 17OCT17 S/N 1177, DETAIL VISUAL INSPECTION (DVI) AND TAP-TEST WAS PERFORMED, ADITIONAL DAMAGE WAS NOT FOUND PER B-717 SRM 57-53-01-1A PAR. 2.B. UP DATE DETAILS: FOR TAP TEST INSPECTION SEE REFERENCE LOG 0037908 PER SRM 57-53-01-1A PAR 2.B (LP #0037896)

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 41,521 hrs · 27,768 cycles

DENT ON LH WING FIXED I/B VANE LOWER SURFACE BTW ATTACH POINTS 2 AND 3 (AI). NR 00014 DENT ON LH WING FIXED I/B VANE LOWER SURFACE BTW ATTACH POINTS 2 AND 3 WAS MEASURED, DENT 1 DIAMETER 0.500" AND DEPTH 0.023" THEREFORE IS WITHIN LIMITS PER B-717 SRM 57-53-01-1A. EQUIPMENT USED, P/N:543-402 VENCE: 17OCT17 S/N 1177; DETAIL VISUAL INSPECTION (DVI) AND TAP-TEST WAS PERFORMED, ADITIONAL DAMAGE WAS NOT FOUND PER B-717 SRM 57-53-01-1A PAR. 2.B. FOR VISUAL INSPECTION SEE REFERENCE LOG 0037933 PER SRM 57-53-01-1A PAR 2.B. (LP #0037937)

Part: SKIN — DENTED (LT WING SPOILER) · airframe 41,521 hrs · 27,768 cycles

DENT ON THE LT WING INBD SPOILER UPPER SURFACE. FOUND TO BE WITHIN LIMITS IAW SRM 57-70-01-1A.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 41,521 hrs · 27,768 cycles

DENT ON LH WING FIXED I/B VANE LOWER SURFACE BTW ATTACH POINTS 2 AND 3 (AI). NR 00014 DENT ON LH WING FIXED I/B VANE LOWER SURFACE BTW ATTACH POINTS 2 AND 3 WAS MEASURED, DENT 1 DIAMETER 0.500" AND DEPTH 0.023" THEREFORE IS WITHIN LIMITS PER B-717 SRM 57-53-01-1A. EQUIPMENT USED, P/N:543-402 VENCE: 17OCT17 S/N 1177; DETAIL VISUAL INSPECTION (DVI) AND TAP-TEST WAS PERFORMED, ADDITIONAL DAMAGE WAS NOT FOUND PER B-717 SRM 57-53-01-1A PAR. 2.B. UP DATE DETAILS: FOR TAP TEST INSPECTION SEE REFERENCE LOG 0037937 PER SRM 57-53-01-1A PAR 2.B. (LP #0037933)

Part: SKIN — DENTED (LT WING) · airframe 41,521 hrs · 27,768 cycles

DENT ON THE LT WING INBD SPOILER UPPER SURFACE. FOUND WITHIN LIMITS IAW SRM 57-70-01-1A.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 41,521 hrs · 27,768 cycles

CRACKED ANGLE ON THE LT AFT EMERGENCY EXIT DOOR AT STOP FITTING 10. THE ANGLE WAS REPLACED IAW DWG #9957735, REV G, SRM 51-41-02, AND 51-41-05.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 41,521 hrs · 27,768 cycles

CRACKED FWD ANGLE JUST ON THE NR 1 BEAM AT FWD OVWERWING EMERGENCY DOOR. THE ANGLE WAS WAS REPLACED IAW DWG 9957735, REV G, SRM 51-41-02, AND 51-41-05.

Part: WINDOW FRAME — CRACKED (BS 870) · airframe 41,521 hrs · 27,768 cycles

CRACKS ON WINDOW PANE, BS 870. THE WINDOW PANE WAS REPAIRED IAW SRM 56-20-02 REPAIR 1.

Part: SKIN — DAMAGED (BS 577-580) · airframe 41,521 hrs · 27,768 cycles

DENT AND SCRAPE IN THE RT SKIN AT BS 577 - 580, BETWEEN STRINGERS 25R - 26R. CLEANED AREA. ACCOMPLISHED HFEC INSPECTION IAW SRM 53-01-01 & AMM NDT SPM 06.10.01.001. NO CRACKS INDICATED. THE DENT WS FOUND TO BE 0.092 DEEP BY 2 INCHES WIDE. IAW SRM 53-01-01, CONDITION 1C, INSPECTION WAS PERFORMED AND INTERNAL DOUBLER EXISTING ON AREA IAW SRM 53-01-01-1A. THE AREA WAS REPAIRED IAW ETI-17-17-065, REV 3, AND ER/A 558133-14, REV ORIGINAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,727 hrs · 24,135 cycles

FWD LT OVERWING DOOR EMER LIGHT INOPERATIVE. RELAMPED IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,727 hrs · 24,135 cycles

AFT LT OVERWING DOOR EMER LIGHT INOPERATIVE. RELAMPED IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,727 hrs · 24,135 cycles

AFT FLIGHT ATTENDANT`S SEAT EMER LIGHT INOPERATIVE. RELAMPED IAW MM.

Part: COVER — CRACKED (CABIN) · airframe 36,727 hrs · 24,135 cycles

ROW 1 CEILING EMER LIGHT COVER CRACKED. R & R COVER IAW MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 35,188 hrs · 23,073 cycles

EMERGENCY LIGHTS BATTERY CHARGER B5 235 INOPERATIVE. R & R BATTERY CHARGER IAW MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 35,188 hrs · 23,073 cycles

EMERGENCY LIGHTS BATTERY CHARGER B5 229 INOPERATIVE. R & R BATTERY CHARGER IAW MM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 35,188 hrs · 23,073 cycles

EMERGENCY LIGHT BATTERY PACK B5-119 INOPERATIVE. R & R BATTERY PACK IAW MM.

Part: PANEL — DELAMINATED (LT SPOILER) · airframe 35,188 hrs · 23,073 cycles

LEFT WING OTBD SPOILER PANEL DELAMINATED. R & R SPOILER PANEL IAW MM.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 35,188 hrs · 23,073 cycles

AFT CARGO FLOOR SUPPORT FITTING CRACKED BETWEEN BS 946 - 954, BETWEEN LONGERON 30R - 29R. R & R FITTING IAW SRM & DWG.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 35,188 hrs · 23,073 cycles

AFT ACCESSORY COMPARTMENT, RT LOUVER FWD LOWER ATTACHMENT CLIP CRACKED. R & R CLIP IAW DWG.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 35,188 hrs · 23,073 cycles

MAIN CABIN FLOORBOARD NR 221JF DELAMINATED. R & R FLOORBOARD IAW DWG & SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 35,188 hrs · 23,073 cycles

MAIN CABIN FLOORBOARD NR 221ARF DELAMINATED. R & R FLOORBOARD IAW DWG & SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 35,188 hrs · 23,073 cycles

MAIN CABIN FLOORBOARD NR 221ATF DELAMINATED. REPAIRED FLOORBOARD IAW DWG & SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 35,188 hrs · 23,073 cycles

MAIN CABIN FLOORBOARD NR 221WF DELAMINATED. R & R FLOORBOARD IAW DWG & SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 35,188 hrs · 23,073 cycles

AFT ACCESSORY COMPARTMENT RT LOUVER UPPER AFT WEB CLIP CRACKED. R & R CLIP IAW DWG.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 35,188 hrs · 23,073 cycles

MAIN CABIN FLOORBOARD NR 221 VF DELAMINATED. R & R FLOORBOARD IAW DWG & SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 35,188 hrs · 23,073 cycles

MAIN CABIN FLOORBOARD NR 221ASF DELAMINATED. R & R FLOORBOARD IAW DWG & SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 35,188 hrs · 23,073 cycles

MAIN CABIN FLOORBOARD NR 221AHF DELAMINATED. R & R FLOORBOARD IAW DWG & SRM.

Part: MOUNT — CORRODED (FUSELAGE) · airframe 35,188 hrs · 23,073 cycles

CABIN AT R1 DOOR JAMB FWD & AFT FLOOR MOUNTS CORRODED. R & R MOUNTS IAW SRM.

Part: PANEL — DELAMINATED (LT SPOILER) · airframe 35,188 hrs · 23,073 cycles

LEFT WING INBD SPOILER PANEL DELAMINATED. R & R SPOILER PANEL IAW MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 36,727 hrs · 24,135 cycles

RIGHT MAIN FRAME CRACKED AT BS 674. R & R FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,188 hrs · 23,073 cycles

MAIN CABIN FRAME CRACKED AT STATION 674, RT SIDE. REPAIRED FRAME IAW SERVICE BULLETIN.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 35,602 hrs · 23,350 cycles

RI DOOR SLIDE OUT OF POSITION. REINSTALLED SLIDE IAW MM.

Part: LATCH — LOOSE (L1 DOOR) · airframe 35,553 hrs · 23,314 cycles

L1 DOOR EMER SLIDE COVER LATCH LOOSE. SECURED LATCH IAW AMM.

Part: COMPRESSOR — DAMAGED (NR 1 ENGINE) · airframe 35,376 hrs · 23,192 cycles

DIVERSION COMPRESSOR STALLED ON CLIMB OUT. FOUND STAGE 4 HPC DAMAGE OUT OF LIMITS NR 1 ENG. R & R THE NR 1 ENG ASSEMBLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,504 hrs · 22,631 cycles

EEPLS INOPERATIVE AT ROW 1. REPAIRED EEPLS IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,533 hrs · 22,650 cycles

LT EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE AT ROW D. RELAMPED LIGHTS IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,533 hrs · 22,650 cycles

RT EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE AT ROW D. RELAMPED LIGHTS IAW MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 34,466 hrs · 22,606 cycles

EMERGENCY LIGHT CHARGER INOPERATIVE AT B5-231. R & R CHARGER IAW.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 32,652 hrs · 21,452 cycles

MAIN CABIN FLOOR PANEL 222 ZF CRACKED AT THE EDGE, MID-WAY OF PANEL. REPAIRED DOUBLER IAW SRM.

Part: FORMER — CRACKED (FUSELAGE) · airframe 32,652 hrs · 21,452 cycles

AFT ACCESSORY COMPARTMENT. FORMER CRACKED AT BS 1152, LONGERON 2R. R & R FORMER IAW SRM & DRAWING.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 32,652 hrs · 21,452 cycles

MAIN CABIN FLOOR PANEL 222YF DELAMINATED. R & R PANEL IAW B717 SRM 53-20-50.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 32,652 hrs · 21,452 cycles

MAIN CABIN FLOOR PANEL 222ADF DELAMINATED. R & R PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 32,652 hrs · 21,452 cycles

FLOOR PANEL 222RF DELAMINATED BETWEEN STATION 541 TO STATION 636. R & R PANEL IAW SRM.

Part: DOUBLER — LOOSE (VERTICAL STAB) · airframe 32,652 hrs · 21,452 cycles

VERTICAL STABILIZER LE DOUBLER LOOSE. REPAIRED DOUBLER IAW DRAWING & EA.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 32,652 hrs · 21,452 cycles

PANEL 222 AEF DELAMINATED BETWEEN STATION 646 TO STATION 737. REPAIRED PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 32,652 hrs · 21,452 cycles

FLOOR PANEL 222TF DELAMINATED BETWEEN STATION 465 TO STATION 541. R & R PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 32,652 hrs · 21,452 cycles

MAIN CABIN STATION 313-389 FLOOR PANEL 221UF DELAMINATED. R & R PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 32,652 hrs · 21,452 cycles

MAIN CABIN FLOOR PANEL 222AAF DELAMINATED BETWEEN STATION 636 TO STATION 674. R & R PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 32,652 hrs · 21,452 cycles

FLOOR PANEL 222APF DELAMINATED BETWEEN STATION 813 TO STATION 889. R & R PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 32,652 hrs · 21,452 cycles

FLOOR PANEL 222ABF DELAMINATED BETWEEN STATION 636 TO STATION 674. R & R PANEL IAW SRM.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 32,652 hrs · 21,452 cycles

MAIN CABIN FLOOR PANEL 22AVF CORRODED BETWEEN STATION 889 TO STATION 954. R & R PANEL IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 32,652 hrs · 21,452 cycles

CUSP CRACKED AT STATION 660, RBL 54. R & R CUSP IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 32,652 hrs · 21,452 cycles

CUSP CRACKED AT STATION 850, RBL 50. REPAIRED CUSP WEB IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 32,652 hrs · 21,452 cycles

CUSP CRACKED AT STATION 650, RBL 54. R & R CUSP WEB IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 32,652 hrs · 21,452 cycles

LT CUSP WEB CRACKED BETWEEN BS 715 TO BS 655, LBL 54. R & R CUSP WEB IAW SRM.

Part: SKIN — CRACKED (RT WING) · airframe 32,652 hrs · 21,452 cycles

RT WING FUELING ACCESS DOOR CUT OUT CRACKED. REPAIRED DOUBLER IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 32,652 hrs · 21,452 cycles

LT WING TO BODY FWD FAIRING SUPPORT GROUND STRAP CRACKED AT BS 636. R & R STRAP IAW SRM & DRAWING.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 32,652 hrs · 21,452 cycles

RT CUSP CORRODED AT STATION 627. R & R CUSP IAW SRM.

Part: BONDING STRAP — CRACKED (RT WING) · airframe 32,652 hrs · 21,452 cycles

RT WING TO BODY BONDING STRAP CRACKED STREAMER ATTACHED. R & R STRAP IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 32,652 hrs · 21,452 cycles

RT CUSP CORRODED BETWEEN STATION 541 TO STATION 560. REPAIRED CUSP WEB IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 32,652 hrs · 21,452 cycles

RT CUSP CORRODED BETWEEN BS 579 TO BS 598. R & R CUSP IAW SRM & DRAWING.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 32,652 hrs · 21,452 cycles

VERTICAL SUPPORT CRACKED BELOW SEAT TRACK & CENTER TANK AT STATION 737, LBL 44. R & R SUPPORT IAW MM.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 32,652 hrs · 21,452 cycles

VERTICAL SUPPORT CRACKED BELOW SEAT TRACK & CENTER TANK AT STATION RBL 44. R & R FITTING IAW SRM & DRAWING.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 32,652 hrs · 21,452 cycles

LT WW AFT BULKHEAD OTBD SIDE BRACKET CRACKED. R & R BRACKET IAW DRAWING & SRM.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 32,652 hrs · 21,452 cycles

LT WW FWD DOOR CUT OUT INBD BRACKET CRACKED. R & R BRACKET IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 32,652 hrs · 21,452 cycles

RT WW FWD VERTICAL DOOR CUT OUT AT THE END CRACKED. REPAIRED ANGLE IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,652 hrs · 21,452 cycles

RT MAIN FRAME CRACKED AT BS 715. R & R FRAME IAW DRAWING & SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 32,652 hrs · 21,452 cycles

FUSELAGE SKIN LOWER WEB CORRODED AT STATION 851, LONGERON 30. REPAIRED SKIN IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,652 hrs · 21,452 cycles

LT MAIN FRAME CRACKED AT BS 674 AT FLOOR BEAM INTERSECTION. R & R FRAME IAW SRM & DRAWING.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 32,652 hrs · 21,452 cycles

LONGERON CRACKED AT BS 1133, LONGERON 2L. REPAIRED LONGERON IAW SRM.

Part: FORMER — CRACKED (FUSELAGE) · airframe 32,652 hrs · 21,452 cycles

FORMER CRACKED AT BS 1144, LONGERON 2R. R & R FORMER IAW DRAWING & SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 32,652 hrs · 21,452 cycles

CLIP CRACKED AT BS 1152, LONGERON 2R. R & R CLIP IAW SRM & DRAWING.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 32,652 hrs · 21,452 cycles

LONGERON CRACKED AT BS 1133, LONGERON 2R. REPAIRED LONGERON IAW SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 34,124 hrs · 22,385 cycles

FUSELAGE SKIN LOWER WING TO BODY CORRODED AT STATION 851, LONGERON 30. REPAIRED DOUBLER IAW SRM.

Part: FORMER — CRACKED (FUSELAGE) · airframe 32,652 hrs · 21,452 cycles

FORMER CRACKED AT BS 696, STRINGER 26L. REPAIRED FORMER IAW SRM & DRAWING.

Part: FORMER — CRACKED (FUSELAGE) · airframe 32,652 hrs · 21,452 cycles

FORMER CRACKED AT STATION 674, STRINGER 25L. R & R FORMER IAW SRM & DRAWING.

Part: PAN — CORRODED (FUSELAGE) · airframe 32,652 hrs · 21,452 cycles

AFT CARGO DOOR FUSELAGE LOWER JAMB CORRODED. R & R JAMB PAN IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 32,652 hrs · 21,452 cycles

MAIN FRAME WING TO FUSELAGE FITTING CRACKED AT STATION 661, LONGERON 22L. R & R FITTING IAW SRM & DRAWING.

Part: FORMER — CRACKED (FUSELAGE) · airframe 32,652 hrs · 21,452 cycles

FORMER CRACKED AT STATION 674, LONGERON 25R. R & R FORMER IAW SRM & DRAWING.

Part: FITTING — CRACKED (FUSELAGE) · airframe 32,652 hrs · 21,452 cycles

MAIN FRAME WING TO FUSELAGE FITTING CRACKED AT STATION 661, LONGERON 22R. R & R FITTING IAW SRM & DRAWING. .

Part: FORMER — CRACKED (FUSELAGE) · airframe 32,652 hrs · 21,452 cycles

FORMER CRACKED AT STATION 715, LONGERON 26L. R & R FORMER IAW DRAWING & SRM.

Part: FORMER — CRACKED (FUSELAGE) · airframe 32,652 hrs · 21,452 cycles

FORMER CRACKED AT STATION 715, LONGERON 26R. R & R FORMER IAW SRM & DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,652 hrs · 21,452 cycles

BELOW CENTER WING TANK AT FRAME CRACKED AT BS 696, LONGERON 26R. R & R FRAME IAW SRM & DRAWING.

Part: SLAT — CRACKED (LT WING) · airframe 32,652 hrs · 21,452 cycles

LT WING LE CRACKED AT PREVIOUS REPAIR RIVET LOCATED UNDER NR 1 SLAT BETWEEN CENTER SLAT TRACK & ANTI-ICE DUCT. REPAIR SLAT IAW SRM.

Part: LANYARD — LOOSE (EVAC SLIDE) · airframe 33,942 hrs · 22,256 cycles

R1 DOOR EMERGENCY EVAC SLIDE LANYARD LOOSE. SECURED LANYARD IAW MM.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 33,558 hrs · 22,011 cycles

EMERGENCY EXIT LIGHT INOPERATIVE BETWEEN ROW 1 TO ROW 20. CONNECTED WIRE CONNECTORS IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,832 hrs · 20,956 cycles

BOTH CLEAR EMERGENCY ESCAPE PATH LIGHT ASSY ON AISLE SIDE SEAT 1D ARE INOP. FOUND SEAT 1D EMERGENCY LIGHTS OPERATE NORMALLY PER AMM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 196, LBL 15 TO LBL 42, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-10-04 AND REF DWG PL 9936534. SEE NR 769033.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 160, LBL 5 TO RBL 5, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-10-04, 53-00-00 AND 51-41-02. SEE NR 769027.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 160 TO 180, RBL 44, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02, 51-41-05. SEE NR 769023.

Part: SEAT TRACK — CORRODED (FUSELAGE)

MAIN CABIN SEAT TRACK, STA 200 TO 256, RBL 22, CORROSION. ACCOMPLISHED SEAT TRACK SPLICE REPAIR PER B717 SRM 53-20-52 FIG 201.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 200, RBL46 TO RBL 57, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-10-04, 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 148 TO 200, LBL 7, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-10-04 AND 51-41-01. SEE NR 769026 AND 769026-1.

Part: SEAT TRACK — CORRODED (BS 200-256)

MAIN CABIN SEAT TRACK, STA 200 TO 256, RBL 44.5, CORRODED. REPAIRED PER SRM 53-20-52 REPAIR 5 FIG 201.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 200, LBL 10, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02.

Part: WEB — CORRODED (FUSELAGE)

CABIN FLOOR WEB, STA 202, RBL 41, CORROSION. ACCOMPLISHED FLOOR WEB REPLACEMENT PER B717 SRM 51-41-02, 51-10-04 AND REF DWG PL 9936535.

Part: WEB — CORRODED (FUSELAGE)

CABIN FLOOR WEB, STA 183, RBL 5, CORROSION. ACCOMPLISHED FLOOR WEB DOUBLER REPAIR PER B717 SRM 51-10-04, 53-00-00 AND 51-70-10. SEE NR 769030 AND 769030-1.

Part: GUSSET — CRACKED (BS 212)

FUSELAGE GUSSET, STA 212, L15, CRACKED. REPAIRED PER B717 51-70-10 REPAIR 2, FIG 201.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 148 TO 200, RBL 7, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 53-00-00 AND 51-41-01. SEE NR 769025 AND 769025-1.

Part: DOOR FRAME — CORRODED (FUSELAGE)

AFT CARGO DOOR JAMB, CORROSION. ACCOMPLISHED DOOR JAMB ANGLE REPAIR PER B717 SRM 51-41-01, 53-20-15, 51-10-04 AND 51-41-02. SEE NR 768926 AND 768926-1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 160 TO 196, LBL 55, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02 AND 51-41-05. SEE NR 769036 AND 769036-1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 200 TO 256, LBL 14, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-10-04, 53-00-00, 51-41-02 AND 51-41-05. SEE NR 769040 AND 769040-1.

Part: STRUCTURE — CORRODED (FUSELAGE)

GALLEY AFT INBOARD SKINS, CORROSION. ACCOMPLISHED AFT INBOARD SKINS DOUBLER REPAIR PER B717 SRM 51-70-10 AND EA 17-25-03545IR. SEE NR 769010 AND 769010-1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 237, BL 0, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-10-04, 53-00-00 AND 51-41-05. SEE NR 769046 AND 769046-1.

Part: FITTING — CORRODED (GIRT BAR)

R1 DOOR FWD AND AFT GIRT BAR FITTINGS, CORROSION. ACCOMPLISHED GIRT BAR FITTINGS REPLACEMENT PER B717 SRM 51-10-04, 53-00-00 AND 51-41-02. SEE NR 768974.

Part: FLOORBEAM — CORRODED (BS 180)

CABIN FLOORBEAM BS 180, RBL 9 TO RBL 43, CORROSION. ACCOMPLISHED FLOORBEAM REPLACEMENT PER SRM 51-41-02.

Part: FLOORBEAM — CORRODED (BS 200)

CABIN FLOORBEAM BS 200, LBL 5 TO RBL 5, CORRODED. ACCOMPLISHED FLOORBEAM REPLACEMENT PER SRM 51-41-02.

Part: FLOORBEAM — CORRODED (BS 200)

CABIN FLOORBEAM BS 200, RBL 9 TO RBL 46, CORROSION. ACCOMPLISHED FLOORBEAM REPLACEMENT PER SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (BS 200-214)

CABIN FLOOR SUPPORT, BS 200-214, RBL 55, CORRODED. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER SRM 51-41-02, 51-4

Part: DOOR FRAME — CORRODED (CARGO DOOR)

FWD CARGO LWR DOOR FRAME CORRODED. ACCOMPLISHED LWR DOOR JAMB SPLICE PER SRM 53-20-15 REPAIR 6, FIG 201.

Part: PANEL — CORRODED (BS 200)

E&E COMPARTMENT UPPER CEILING PANEL, BS 200, CORRODED. ON. ACCOMPLISHED UPPER CEILING PANEL REPLACEMENT PER SRM 51-41-02.

Part: LIGHT — INOPERATIVE (COCKPIT)

FLIGHT DECK EMERGENCY LIGHT HAS ONE BULB INOP. RELAMPED FLIGHT DECK EMERGENCY LIGHT. OPS CHECKED GOOD REF AMM 33-51-11.

Part: WIRE — BROKEN (CABIN)

ROW 27 SEAT EMERGENCY LIGHT INOP. FOUND BROKEN WIRE FROM PLUG. REMOVED AND REPLACED CONNECTOR. OPS CHECK GOOD IAW B717 SWPM 20-31.

Part: SIGN — LOOSE (CABIN)

EXIT SIGN ABOVE ROW 1 IS LOOSE. SECURED THE EXIT SIGN ABOVE SEAT ROW 1 IN PLACE IAW AMM 33-50.

Part: CONNECTOR — LOOSE (CABIN)

BOTH EMERGENCY ESCAPE PATH LIGHTS ON SIDE OF SEAT 1D ARE INOP. SECURED CONNECTOR ON SEAT 1D. CHECKS GOOD. REF MM 33-51.

Part: FRAME — CORRODED (FUSELAGE)

AFT CARGO COMPARTMENT FRAME, STA 870, LONG L29L TO L30, CORROSION. ACCOMPLISHED FRAME BLENDING WITHIN LIMITS PER B717 SRM 51-10-01 AND B717 SRM 51-22-01.

Part: FRAME — CORRODED (FUSELAGE)

AFT CARGO COMPARTMENT FRAME, STA 974, LONG L30, CORROSION. ACCOMPLISHED FRAME BLENDING WITHIN LIMITS PER B717 SRM 51-10-01 AND B717 SRM 53-00-00 FIG 103.

Part: LONGERON — CORRODED (FUSELAGE)

AFT CARGO COMPARTMENT LONGERON SECTION, STA 927 TO 974, LONG L28L, CORROSION. ACCOMPLISHED LONGERON SECTION BLENDING WITHIN LIMITS PER B717 SRM 51-10-01 AND B717 SRM 53-00-00 FIG 103.

Part: SKIN — CORRODED (FUSELAGE)

AFT CARGO COMPARTMENT FUSELAGE SKIN, STA 954 TO 974, LONG L28R TO L29R, CORROSION. ACCOMPLISHED FUSELAGE SKIN BLENDING WITHIN LIMITS PER B717 SRM 51-10-01 AND B717 SRM 51-22-01.

Part: FRAME — CORRODED (FUSELAGE)

AFT CARGO COMPARTMENT FRAME, STA 851, LONG L29L TO L29R, CORROSION. ACCOMPLISHED FRAME BLENDING WITHIN LIMITS PER B717 SRM 51-10-01 AND B717 SRM 51-22-01.

Part: LONGERON — CORRODED (FUSELAGE)

AFT CARGO COMPARTMENT LONGERON SECTION, STA 954, LONG L30, CORROSION. ACCOMPLISHED LONGERON SECTION BLENDING WITHIN LIMITS PER B717 SRM 51-10-01 AND B717 SRM 51-41-02.

Part: FRAME — DAMAGED (FUSELAGE)

EO 17-5310-2895 AFT RIGHT STA 1178 CANTED FRAME INSPECTION IDENTIFIED CONFIGURATION 2 CONDITION 2. ACCOMPLISHED REPAIR TO AFT FUSELAGE FRAME CAP, CANTED STA 1178.225, RIGHT SIDE IAW TASK CARD 17-5310-2987.

Part: DOOR FRAME — CORRODED (CARGO BAY)

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

Part: FRAME — CORRODED (FUSELAGE)

AFT CARGO COMPARTMENT FRAME, STA 927, LONG L29L, CORROSION. ACCOMPLISHED FRAME BLENDING WITHIN LIMITS PER B717 SRM 51-10-01.

Part: FRAME — DAMAGED (FUSELAGE)

EO 17-5310-2937 AFT LEFT STA 1178 CANTED FRAME INSPECTION IDENTIFIED CONFIGURATION 2 CONDITION 2. ACCOMPLISHED REPAIR TO AFT FUSELAGE FRAME CAP, CANTED STA 1178.225, LEFT SIDE IAW TASK CARD 17-5310-2977.

Part: DOOR FRAME — CORRODED (CARGO BAY)

FWD CARGO DOOR JAMB PAN, CORROSION. ACCOMPLISHED JAMB PAN BLENDING WITHIN LIMITS PER B717 SRM 51-10-04 AND B717 SRM 53-00-00 FIG 103.

Part: PIN — LOOSE (CONNNECTOR)

EMERGENCY LIGHTS AT ROW 1 2 EACH INOPERATIVE. FOUND LOOSE PIN FOR CONNECTOR UNDER SEAT. RE-ALIGNED & OPS CHECK GOOD IAW WDM SP.

Part: WARNING SYSTEM — MALFUNCTIONED (MLG)

AFTER LANDING GEAR EXTENSION WAS SELECTED, RECEIVED A "GEAR DOOR OPEN" INDICATION AFTER THE MLG WAS DOWN AND LOCKED. AIRCRAFT FERRIED TO ATL. ATL MAINTENANCE PERFORMED INSPECTION AND OPS CHECKS WITH GEAR SWINGS. COULD NOT DUPLICATE THE PROBLEM. NO DEFECTS NOTED.

Part: SLIDE — UNSERVICEABLE (R1 DOOR)

R-1 DOOR SLIDE PRESSURE NOT IN GREEN BAND. REMOVED AND REPLACED R-1 DOOR SLIDE IN REF TO ATM 25-61-03.

Part: UNKNOWN — ODOR

ON SHORT FINAL APPROACH ELECTRICAL FIRE ODOR DETECTED, RADAR TURNED OFF, PREDICTIVE WIND SHEAR FAIL ALERT BECAME DISPLAYED AFTER LANDING BAD POWER TRANSFER BREAK OCCURRED WHEN RIGHT ENGINE SHUTDOWN AFTER THREE MINUTES COOL DOWN PERIOD. PERFORMED WX TEST IAW 717 AMM 34-41-00 NO CURRENT DEFECTS NOTED. INSPECTED WX RT AND ANTENNA, NO ODORS DETECTED IN COMPARTMENT, OPERATED PARTS, NO ODOR DETECTED.

Part: CONNECTOR — NOT SEATED (PSU)

DURING MANUAL EJECT TEST OF OXYGEN MASKS, PSU 15 AC AND 30 DEF DID NOT DEPLOY. ON INSPECTION FOUND CONNECTORS NOT SEATED ALL THE WAY, RESEATED CONNECTORS AT SWITCH. OPERATION TEST NORMAL IAW AMM 35-22-06.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

E-PATH LIGHTS ON SEATS 1, 2, 3, AND 10D WILL NOT ILLUMINATE. REMOVED AND REPLACED BATTERY PACK ASSY IAW B717 M/M 33-51, OPS CHECK GOOD.