N932AT

Part: NONE — NONE (NONE) · airframe 55,615 hrs · 40,241 cycles

DTA ER/A 628389-14 SECTION II MONITOR LOG REQUIRES DTA APPROVAL ON OR BEFORE THE NEXT 24 MONTHS AFTER 04-SEP-25. CORRECTIVE ACTION: REPAIRED ASSOCIATED ER/A 00-628389 (1183511)

Part: NONE — NONE (NONE) · airframe 55,615 hrs · 40,241 cycles

DTA ER/A 628285-14 SECTION II MONITOR LOG REQUIRES DTA APPROVAL ON OR BEFORE THE NEXT 24 MONTHS AFTER 24-AUG-25. DISCONTINUE REVENUE SERVICE ON OR BEFORE THE NEXT 24 MONTHS AFTER 24-AUG-25 PENDING A DAMAGE TOLERANCE AND FATIGUE REVIEW. ASSOCIATED ER/A 00-628285 (1165214)

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 55,615 hrs · 40,241 cycles

SHIP 9568 INITIAL INSPECTION: CRACKED FRAME CLIP ON STA Y=1144 BTW LONG 1 AND LONG 2L ALSO ON STA Y=1152 BTW LONG 1 AND LONG 2L AT AFT ACC . COMPARTMENT. CORRECTIVE ACTION: REPAIRED PER ER/A 626274-14 REV. (0990391)

Part: LONGERON — CRACKED (ZONE 200) · airframe 55,615 hrs · 40,241 cycles

SHIP 9568 INITIAL INSPECTION: CRACK ON LONG 2 LH STA Y=1133 AT AFT ACC COMPARTMENT. CORRECTIVE ACTION: REPAIRED PER B717-200 SRM 53-00-05-2R REPAIR 2 (0967936)

Part: TAB — DELAMINATED (LT AILERON) · airframe 55,615 hrs · 40,241 cycles

SHIP 9568 INITIAL INSPECTION: DELAMINATED CONTROL TAB OF AILERON AT LH WING. CORRECTIVE ACTION: AILERON CONTROL TAB WAS REMOVED (PN: UNK, SN: 5106) AND SERVICEABLE AILERON CONTROL TAB (P/N: 5910047-501 S/N: 5029) WAS INSTALLED AT LH WING PER B717-200 AMM 27-10-02. (0951935)

Part: ACCESS PANEL — LEAKING (ZONE 500) · airframe 55,611 hrs · 40,240 cycles

-AD- FUEL LEAK FOUND DURING INSPECTION OF THE LH WING AFT LOWER SKIN DOUBLER AT XRS=164. CONTACT LIAISON ENG FOR REPAIR PROCEDURES PRIOR TO FURTHER FLIGHT AA #FE5720-011.03. ALL REPAIRS C/W PER ERA 622371-14AD. RII C/W [DELTA QC5223]. (LP #0903374)

Part: SKIN — LEAKING (ZONE 500) · airframe 55,611 hrs · 40,240 cycles

-AD- FUEL LEAK FOUND DURING INSPECTION OF THE LH WING AFT LOWER SKIN AT XRS=164 AA #FE5720-01103. ALL REPAIRS C/W PER ERA 622371-14AD. RII C/W [DELTA QC 5223]. (LP #0903380)

Part: ATTACH FITTING — CRACKED (ZONE 500) · airframe 55,611 hrs · 40,240 cycles

-AD- PRI 622371-14AD, REV 2 HOLE #6 ON INBOARD FLAP FAIRING ATTACH BRACKET HAS CRACK INDICATION. FLAP FAIRING ATTACH BRACKET REPLACED DURING LEFT WING LOWER SKIN DOUBLER REPAIR ON ER/A 622371-14AD, REV O. JOB COMPLETE. A/C OK FOR SERVICE. (LP #0803565)

Part: ATTACH BRACKET — CRACKED (ZONE 500) · airframe 55,611 hrs · 40,240 cycles

-AD- PRI 622371-14AD, REV 3 HOLE #9 ON OUTBOARD FAIRING ATTACH BRACKET HAS CRACK INDICATION. FLAP FAIRING ATTACH BRACKET REPLACED DURING LEFT WING LOWER SKIN DOUBLER REPAIR ON ER/A 622371-14AD, REV O. JOB COMPLETE. A/C OK FOR SERVICE. (LP #0803598)

Part: ATTACH FITTING — CRACKED (ZONE 500) · airframe 55,611 hrs · 40,240 cycles

-AD- PRI 622371-14AD, REV 2 HOLE #5 ON INBOARD FLAP FAIRING ATTACH BRACKET HAS CRACK INDICATION. FLAP FAIRING ATTACH BRACKET REPLCAED DUEING LEFT WING LOWER SKIN DOUBLER REPAIR ON ER/A 622371-14AD, REV O. JOB COMPLETE. A/C OK FOR SERVICE. (LP #0803562)

Part: ATTACH BRACKET — CRACKED (ZONE 500) · airframe 55,611 hrs · 40,240 cycles

-AD- PRI 622371-14AD, REV 3 HOLE #5 ON OUTBOARD FLAP FAIRING ATTACH BRACKET HAS CRACK INDICATION. FLAP FAIRING ATTACH BRACKET REPLACED DURING LEFT WING LOWER SKIN DOUBLER REPAIR ON ER/A 622371-14AD, REV O. JOB COMPLETE. A/C OK FOR SERVICE. (LP #0803588)

Part: ATTACH BRACKET — CRACKED (ZONE 500) · airframe 55,611 hrs · 40,240 cycles

-AD- PRI 622371-14AD, REV 3 HOLE #1 ON OUTBOARD FLAP FAIRING ATTACH BRACKET HAS CRACK INDICATION. FLAP FAIRING ATTACH BRACKET REPLACED DURING LEFT WING LOWER SKIN DOUBLER REPAIR ON ER/A 622371-14AD, REV O. JOB COMPLETE. A/C OK FOR SERVICE. (LP #0803577)

Part: ATTACH BRACKET — CRACKED (ZONE 500) · airframe 55,611 hrs · 40,240 cycles

-AD- PRI 622371-14AD, REV 3 HOLE #8 ON OUTBOARD FLAP FAIRING ATTACH BRACKET HAS CRACK INDICATION. FLAP FAIRING ATTACH BRACKET REPLACED DURING LEFT WING LOWER SKIN DOUBLER REPAIR ON ER/A 622371-14AD, REV O. A/C OK FOR SERVICE. (LP #0803594)

Part: ATTACH BRACKET — CRACKED (ZONE 500) · airframe 55,611 hrs · 40,240 cycles

-AD- DURING BHEC ON PRI 622371-14AD, REV 2 HOLE #2 ON INBOARD FLAP FAIRING ATTACH BRACKET HAS A CRACK INDICATION. FLAP FAIRING ATTACH BRACKET REPLACED DURING LEFT WING LOWER SKIN DOUBLER REPAIR ON ER/A 622371-14AD, REV O. JOB COMPLETE. A/C OK FOR SERVICE. (LP #0791086)

Part: SUPPORT FITTING — DAMAGED (ZONE 500) · airframe 55,611 hrs · 40,240 cycles

-AD- ON LEFT WING XRS 164.00 LOWER FLAP HINGE SUPPORT FITTING 2ND NUT FORWARD ON INBOARD SIDE IS LOOSE. FASTENER REPLACED DURING LEFT WING LOWER SKIN REPAIR ON ER/A 622371-14AD, REV O. JOB COMPLETE. A/C OK FOR SERVICE. (LP #0791075)

Part: ATTACH BRACKET — DAMAGED (FLAP FAIRING) · airframe 55,611 hrs · 40,240 cycles

-AD- DURING BHEC ON PRI 622371-14AD, REV 2 HOLE #4 ON INBOARD FLAP FAIRING ATTACH BRACKET HAS CRACK INDICATION. HOLE #4 OVERSIZED TO 0.363" ON STEP 41 OF PRI 622371-14AD, REV 9. FREEZE PLUG INSTALLED ON PART C, STEP 12 OF PRI 622371-14AD, REV 13. HOLE WILL BE PICKED UP AND FASTENER INSTALLED ON LEFT WING LOWER SKIN DOUBLER REPAIR ON ER/A 622371-14AD, REV O. JOB COMPLETE. A/C OK FOR SERVICE. (LP #0791105)

Part: ATTACH BRACKET — DAMAGED (FLAP FAIRING) · airframe 55,611 hrs · 40,240 cycles

-AD- DURING BHEC ON PRI 622371-14AD, REV 2 HOLE #3 ON INBOARD FLAP FAIRING ATTACH BRACKET HAS 2 CRACK INDICATIONS. HOLE #3 OVERSIZED TO 0.547" ON STEP 41 OF PRI 622371-14AD, REV 9. FREEZE PLUG INSTALLED IN HOLE #3 ON STEP 12, PART C OF PRI 622371-14AD, REV 13. HOLE WILL BE PICKED UP AND FASTENER INSTALLED ON LEFT WIGN LOWER SKIN DOUBLER REPAIR ON ER/A 622371- 14AD, REV O. JOB COMPLETE. A/C OK FOR SERVICE. (LP #0791094)

Part: SPAR CAP — DAMAGED (ZONE 500) · airframe 55,611 hrs · 40,240 cycles

-AD- ON UPPER LEG OF LEFT WING AFT SPAR LOWER SPAR CAP XRS 164.00 FASTENER ABOVE INBOARD LOWER FLAP FITTING ATTACH BOLT IS LOOSE AND SPINNING. THIS FASTENER REPLACED WITH OVERSIZE FASTENER DURING LEFT WING SKIN DOUBLER RFEPAIR ON ER/A 622371-14AD, REV O. JOB COMPLETE. A/C OK FOR SERVICE. (LP #0791066)

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 54,566 hrs · 39,327 cycles

THE EMERGENCY LIGHT COVER BY THE FWD LAVATORY IS MISSING. MAINTENANCE INSTALLED THE CEILING LENS REF B717 AMM 33-51. (LP #6015231)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,428 hrs · 38,361 cycles

THERE ARE 3 INOPERATIVE EMERGENCY LIGHTS IN THE AFT WALKWAY. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY, B5-260, REF B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT IS OK FOR SERVICE. (LP #4179381)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 52,457 hrs · 37,581 cycles

ON SERVICE CHECK, THE EMERGENCY LIGHT ABOVE THE FWD FLIGHT ATTENDANT SEAT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY BATTERY POWER SUPPLY PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT IS OK FOR SERVICE. (LP #4731340)

Part: SKIN — CRACKED (BS 1087 S14-15L) · airframe 51,594 hrs · 36,834 cycles

CRACK ON EXTERNAL FUSELAGE SKIN STA Y=1087 BTW LONGERONS 14LH AND 15LH. SUMMARY OF NRC 00141: EXTERNAL FUSELAGE SKIN STA Y=1087 BTW LONGERONS 14LH AND 15LH WAS REPAIRED PER ER/A 605226-14 REV. ORIGINAL SECTION I: TEMPORARY REPAIR. ASSOCIATED ER/A 14-605226 ADDED FOR AC 9568. (LP #2601713)

Part: LONGERON — DAMAGED (BS 1002-1005) · corrosion level 2 · airframe 51,594 hrs · 36,834 cycles

(UT) THICKNESS MEASUREMENT INSPECTION WAS ACCOMPLISHED ON LONGERON STA Y=1002 AND STA Y=1005. ORIGINAL THICKNESS WAS 0.080 INCHES AND REMAINING THICKNESS IS 0.058 INCHES. THEREFOR AREA IS OUT LIMITS IAW SRM 53- 00-00-1A AT AFT CARGO COMPARMENT. CORROSION LEVEL 2. LONGERON 29L REPAIRED IAW SRM 53-00-05-2R PROCEDURE 3 FIG. 201.

Part: CUSP WEB — CRACKED · airframe 51,594 hrs · 36,834 cycles

AD RELATED, RII. HIDDEN DISCREPANCY IN REF AMDS 5310-01436-01C-RH OVERWING FRAME: DURING A/C RH SIDE RETURN TO NORMAL CONDITION, THE CUSP MEMBRANE WAS FOUND CRACKED ON STA Y=715-718 UNDER RH SEAT TRACK X=44.5 AT FLOOR STRUCTURE. SUMMARY OF NRC 249: CUSP WEB WAS REPAIRED PER B717-200 SRM 53-00 -00-2R PROCEDURE 2 PAR 4 A (2). ASSOCIATED AA 5310-01436 ADDED FOR AC 9568. (LP #2589939)

Part: DOUBLER — CORRODED (CARGO DOOR FRAME) · corrosion level 2 · airframe 51,594 hrs · 36,834 cycles

CORROSION ON REPAIR DOUBLE OF AFT CARGO COMPARTMENT DOORJAMB STA Y=954 BTW LONGERONS 26RH AND 27RH. SUMMARY OF NRC 00162: CORROSION LEVEL 2. REPAIR DOUBLE OF AFT CARGO COMPARTMENT DOORJAMB STA Y=954 BTW LONGERONS 26RH AND 27RH WAS REPLACED PER B717-200 SRM 51-41-02-0G STEP 12, B717-200 SRM 51-41-05-0G STEP 8, AND B717-200 SRM 51-41-07-0G STEP 7. (LP #2585517)

Part: NONE — NONE · airframe 50,974 hrs · 36,263 cycles

THE GIRT BAR CABLE DISCONNECTED ON DOOR 1L. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE RESECURED L1 DOOR ESCAPE SLIDE GIRT BAR PER B717 AMM 25-61. (LP #8954222)

Part: POWER SUPPLY — UNSERVICEABLE · airframe 50,169 hrs · 35,519 cycles

FOUND THE LEFT AND RIGHT FORWARD OVERWING LOWER EXIT IDENTIFIERS INOPERATIVE. TROUBLE SHOT PER B717 FIM 33-50-00-810-801, AND FOUND A LOOSE GROUND ON THE RIGHT HAND SIDE EXIT LIGHT. ALSO FOUND B5-118 BATTERY TO BE BAD. REPLACED BATTERY PER B717 AMM 33-51. ALSO FOUND B5-121 BATTERY AND POWER SUPPLY BAD, REPLACED BATTERY AND POWER SUPPLY PER B717 AMM 33-51 AND B717 WDM 33-51-14 SHEET 1. ALL LIGHTS OPERATIONAL CHECKS WERE GOOD. (LP #8651069)

Part: NONE — NONE · airframe 49,931 hrs · 35,304 cycles

SHIP 9568 - THE TAKEOFF WAS ABORTED AT 100-110 KTS. DUE TO A "STICK PUSHER FAIL" MESSAGE AND AIRSPEED INDICATION PROBLEMS. CORRECTIVE ACTION: MAINTENANCE REPLACED THE FORWARD RUDDER LIMITER MOISTURE SUMP ASSEMBLY, PERFORMED PITOT STATIC LEAK CHECK, AND RETURNED THE AIRCRAFT TO SERVICE. (LP #7882396)

Part: BATTERY PACK — INOPERATIVE · airframe 49,864 hrs · 35,250 cycles

THE FWD LEFT & RIGHT OVERWING IDENTIFIEDS EMEGRENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AT R5-121 PER B717 AMM 33-51, OPERATIONAL CHECK WAS GOOD. (LP #7882366)

Part: SKIN — DAMAGED · airframe 49,850 hrs · 35,238 cycles

FOUND FUSELAGE DAMAGE AFT OF L1 BETWEEN F.S. 229-F.S. 256 AT STRS 16L-18L. DAMAGE IS .550 DEEP AT DEEPEST POINT. 11 1/2 IN LONG X 7 IN WIDE AT THE DEEPEST POINT AND 5 IN WIDE AT F.S. 237. REMOVED DAMAGED OUTER SKIN REPAIR AND AFT INTERNAL DOUBLER AND FINGER DOUBLER. REPAIRED SKIN DAMAGE FS 229-FS256 AT STRS 16L-18L PER B717 SRM 53-00-01 REPAIR 6. (LP #2173002)

Part: NONE — NONE · airframe 49,219 hrs · 34,682 cycles

THE AFT CABIN EXIT IDENTIFIER LIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY (B5-119). OPERATIONAL CHECK WAS GOOD. (LP #8120797)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 48,681 hrs · 34,176 cycles

THE AFT EMERGENCY LIGHT ILLUMINATED. MAINTENANCE REPLACED THE BATTERY ASSEMBLY AND BATTERY CHARGER PER B-717 AMM 33-51. OPERATIONAL CHECK WAS NORMAL. AIRCRAFT WAS RETURNED TO SERVICE. (LP #7336354)

Part: LANYARD — OUT OF POSITION (L1 DOOR) · airframe 47,184 hrs · 32,845 cycles

THE L1 DOOR SLIDE LANYARD WAS FOUND TO INSTALLED IMPROPERLY. MAINTENANCE REROUTED THE L1 DOOR SLIDE LANYARD PER B717 AMM 25-61. (LP #7154074)

Part: COVER — MISSING (CABIN) · airframe 44,631 hrs · 30,902 cycles

THE EMERGENCY EXIT LIGHT COVER ABOVE L-1 DOOR IS MISSING. MAINTENANCE REPLACED THE EMERGENCY EXIT LIGHT COVER AT ABOVE L-1 DOOR IAW AMM 33-51. OPERATIONAL CHECK WAS NORMAL. (LP #4290378)

Part: SKIN — DENTED (TE FLAP VANE) · airframe 44,656 hrs · 30,920 cycles

INITIAL INSPECTION- DENTS (2EAS) ON RT AFT MOVABLE VANE LWR SKIN. TWO DENTS LOCATED AT RT AFT MOVABLE VANE LWR SKIN. DENT NR 1 WAS FOUND WITH DISBOND (4"X 1.5") DENT NR 2 DOES NOT HAVE DISBOND PER SRM 51-70 -02-0G PARAG 8.A.(2) AND NDTSPM PART 5, 05-10-02.001. THEREFORE THE DENT NR 1 WAS REPAIRED PER SRM 57-53-01-2R-1 AND SRM 51-70-02-0G AND (VT) (DVI) & (UT) TAP-TEST INSPECTION WERE ACCOMPLISHED AND NO DISBONDS WERE FOUND AFTER REPAIRED AREA PER SRM 51-70-02-0G-2 PAR.16A & NDTSPM PART 5 05-10-02.001. PERFOM DECAL CONDITION EVERY C CHECK PER TOPP 30-10-70 PAR I PAGE 14. (LP0976033)

Part: SKIN — DENTED (TE FLAP VANE) · airframe 44,656 hrs · 30,920 cycles

INITIAL INSPECTION- SEVERAL DENTS ON LT AFT MOVABLE VANE LWR SKIN FOUND ON DENTED AREAS PER SRM 57-53-01-1A-1 PAR.2.B. & NDTSPM PART 5, 05-10-02.001 THEREFORE THE DENTS WERE REPAIRED PER SRM 57-53-01-2R-1 AND SRM 51-70-02-0G AND GVI WAS PERFORMED AT PERIPHERY OF DOUBLER AND NOT DAMAGE WAS FOUND PER SRM 51-70-02-0G PAR 16 A(1). AND (UT)(TAP TEST) WAS PERFORMED ON REPAIRED AREA NO DISBONDS WERE FOUND PER SRM 51-70-02-0G PAR 16 A(3). PERFOM DECAL CONDITION EVERY C CHECK PER TOPP 30-10-70 PAR I PAGE 14. (LP0976052)

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 44,591 hrs · 30,863 cycles

DELAMINATION ON CABIN FLOOR PANELS #223DF, 222RF, 222QF, 221VF, 221RF, AND 222YF. (FUS). NRC 00347: FLOOR PANELS #223DF, 222QF, 221RF, 222RF, AND 221VF WERE FABRICATED, REPLACED, AND IDENTIFIED PER SRM 50-20-50-2R-3. FLOOR PANEL 222YF WAS REINSPECTED (GVI) AND TAP TEST WAS PERFORMED AND NO DAMAGE WAS FOUND PER AMM 05-21-02 210-802. (LP #0965521)

Part: SKIN — CRACKED (CARGO DOOR) · airframe 44,591 hrs · 30,863 cycles

CRACKS ON SKIN AFT BEAM 3 AND 4 AT FWD CARGO DOOR (C1). NRC 00411: CRACKS ON SKIN AFT BEAM 3 AND 4 AT FWD CARGO DOOR (C1) WERE REPAIRED PER SRM 52-30-02-2R REPAIR 3. (LP #0963856)

Part: LONGERON SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,591 hrs · 30,863 cycles

CORROSION ON LONGERON SPLICE BTW STA Y=954 AND Y=974 AT LONGERON 30 AT AFT CARGO COMPARTMENT (CCT). NRC 00105: CORROSION LEVEL 2, FOUND IT IS OUT OF LIMITS PER SRM 53-00-00-01 FIG 103. SPLICE ON LONG BTW STA Y=954 AND Y=974 AT LONGERON 30 AT AFT CARGO COMPARTMENT WAS REPLACED PER SRM 51-40-02 AND 53-20-05-2R-1. (LP #0963446)

Part: FITTING — CRACKED (AFT CARGO DOOR) · airframe 44,591 hrs · 30,863 cycles

CRACKS ON FITTING INTERNAL ON FWD EDGE AT AFT CARGO DOOR. NRC 00334: FITTING WAS FABRICATED AND REPLACED PER DWG #3914025 REV. C AND B717-200 SRM 51-41-05-0G. (LP #0962749)

Part: FLOOR PANEL — BROKEN (CABIN) · airframe 44,591 hrs · 30,863 cycles

BROKEN ON CABIN FLOOR PANELS #222AUF, 222WF, AND 223GF (FUS). NRC 00350: FLOOR PANELS #222AUF AND 223GF WERE FABRICATED, REPLACED, AND IDENTIFIED PER B-717-200 SRM 50-20-50-2R-3: FLOOR PANEL #222WF WAS REINSPECTED (GVI) PER B717-200 AMM 05-21-02 210-802 AND FOUND TO BE NOT BROKEN BUT MISSING THE ADHESIVE AT INSERT AREAS. ADHESIVE WAS APPLIED PER B717-200 SRM 50-20-50-2R-3. (LP #0962997)

Part: FITTING — CRACKED (AFT CARGO DOOR) · airframe 44,591 hrs · 30,863 cycles

CRACKS ON FITTING INTERNAL AT BEAM #4 ON AFT EDGE AT AFT CARGO DOOR. NRC 00394: FITTING WAS FABRICATED AND REPLACED PER DWG #3914025 REV. C AND B717-200 SRM 51-41-05-0G. (LP #0962994)

Part: CUSP WEB — CRACKED (BS 617-636) · airframe 44,591 hrs · 30,863 cycles

CRACK ON CUSP MEMBRANE BEETWEN STA 636 TO 617 LH CABIN PAX FLOOR SIDE. NRC 00154: CRACK ON CUSP MEMBRANE BEETWEN STA 636 TO 617 WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4-04 FIG 216. (LP #0960620)

Part: SKIN — CRACKED (FWD CARGO DOOR) · airframe 44,591 hrs · 30,863 cycles

DURING REMOVAL FITTING ON AFT BEAM #5, CRACKED SKIN AT FWD CARGO DOOR WAS FOUND (IN REFERENCE NRC 332). NRC 00346: CRACKED SKIN AT AFT BEAM #5 FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R REPAIR 3 PAR. 5 FIG. 201. (LP #0961255)

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,591 hrs · 30,863 cycles

CORROSION ON CUSP WEB STA Y=940 TO 942 AND Y=542 TO 544 BTW X=-54 TO X=-44. CORROSION LEVEL 2, CUSP MEMBRANE STA Y=940 TO 942 AND Y=542 TO 544 BTW X=-54 TO X=-44 WERE REPAIRED PER SRM 53-00-55-2R-4 FIGURE 15.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 44,591 hrs · 30,863 cycles

CRACKS ON GENERATION FLOOR PANEL #222NF, 222XF, 222AFF, 221TF, 222ALF, 222ZF, 222EF, AND 222AJF. NRC 00345: CRACKED GENERATION FLOOR PANELS #222NF, 222XF, 222AFF, 221TF, 222ALF, 222ZF, 222EF, AND 222AJF WERE REPAIRED PER BOEING 717-200 SRM 53-20-50-2R-5. (LP #0959470)

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,591 hrs · 30,863 cycles

CRACKS ON SKIN (CUT OUT INTERNAL) 2 EA ON FWD EDGE AND 1 EA AFT EDGE AT FWD CARGO DOOR. NRC 00332: INNER PAN ON FWD EDGE AND AFT EDGE WAS REPAIRED PER SRM 51-30-02-2R REPAIR 1 FIG 201. (LP #0959483)

Part: TRAY — CORRODED (WASTE WATER) · corrosion level 2 · airframe 44,591 hrs · 30,863 cycles

CORROSION ON WATER WASTE TRAY (FUS). NRC 00083: CORROSION LEVEL 2,(UT) WAS ACCOMPLISHED PER NDT SPM 04-00-07, PAR. 5, FIG. 3, SHEET 1-2. ORIGINAL THICKNESS ON WATER WASTE TRAYIS 0.071" AND MINIMUM REMAINING THICKNESS FOUND IS 0.020" THEREFORE IT IS OUT LIMITS PER B717-200 SRM 53-00-00-1A FIG. 103. PANAMETRICS P/N: 389DLP-905M-U-MT-EES, S/N: 140940908 EXP.DATE: 16NOV19, TRANSDUCER: V-260-RM S/N: 913342PAN WATER WASTE TRAY WAS REPLACED PER B717-200 SRM 51-40-02 AND 51-41-05. (LP #0958111)

Part: CUSP WEB — CRACKED (BS 813-832) · airframe 44,591 hrs · 30,863 cycles

CRACK ON CUSP MEMBRANE BEETWEN STA 813 TO 832 RH CABIN PAX FLOOR. NRC 00149: CUSP MEMBRANE BEETWEN STA 813 TO 832 RH CABIN PAX FLOOR AREA WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4-7037. (LP #0955758)

Part: PAN — CRACKED (BS 756-775) · airframe 44,591 hrs · 30,863 cycles

CRACK ON RING PAN BETWEEN STA 756 AND 775 AND STRINGER 14 AND 15 AT RH CABIN PAX. NRC 00265: CRACK ON RING PAN BETWEEN STA 756 AND 775 AND STRINGER 14 AND 15 AT RH CABIN PAX WAS REPAIRED PER BOEING 717-200 SRM 56-20-02-2R-1- FIGURE 202 DETAIL E. (LP #0948837)

Part: RETAINER — BROKEN (TAIL SLIDE COVER) · airframe 41,664 hrs · 28,897 cycles

TAIL SLIDE COVER RETAINER BROKEN. REPLACED THE RETAINER. OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMEGENCY LIGHTS) · airframe 41,101 hrs · 28,532 cycles

BOTH AFT (RT & LT) OVERWING EMERGENCY EXIT CABIN LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE AFT OVERWING EMERGENCY LIGHT BATTERY IAW AMM 33-51. THE AIRCRAFT IS OK FOR SERVICE.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 41,085 hrs · 28,522 cycles

VERTICAL STAB VSS 52, UPPER ROWS EIGHT FASTENERS COUNTERSINK HOLE OVERSIZED. REPAIRED THE VERTICAL STAB SKIN IAW SRM 55-30-01-2R-6, REPAIR 6, AND DWG SG95550001, REV ORIG.

Part: SKIN — DAMAGED (VERTICAL STAB LE) · airframe 41,085 hrs · 28,522 cycles

VERTICAL STAB HAS 4 FASTENER HOLES WORN OUT OF LIMITS AT LEADING EDGE. REPAIRED IAW SRM 55-30-01-2R-6, REPAIR 6, AND DWG SG95550001, REV ORIG.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 40,415 hrs · 28,052 cycles

WHILE PERFORMING A SERVICE CHECK, FOUND FIRST CLASS OVERHEAD CEILING LIGHTS, EMERGENCY LIGHTS INOPERATIVE. INSTALLED A NEW BATTERY IAW AMM 33-51 OPS CHECKED OK. OK FOR SERVICE.

Part: SPOILER — DELAMINATED (RT WING)

DURING UNSCHEDULED MAINTENANCE CHECK RT I/B SPOILER FOUND DELAMINATED.

Part: SKIN — DELAMINATED (LT WING SPOILER)

DURING AN UNSCHEDULE MAINTENANCE CHECK, LT INBD SPOILER FOUND DELAMINATED.

Part: SKIN — DELAMINATED (LT SPOILER)

DURING UNSCHEDULE MAINTENANCE CHECK LT INBD SPOILER WAS FOUND DELAMINATED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,633 hrs · 25,979 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING IN THE TAIL COMPARTMENT WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: SIGN — LOOSE (ROW 1) · airframe 36,618 hrs · 25,127 cycles

OVERHEAD EMERGENCY LIGHT MOUNT BRACKET BROKEN ABOVE ROW 1. R & R SIGN ASSEMBLY IAW MM.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 36,618 hrs · 25,127 cycles

TAIL COMPARTMENT AFT EMERGENCY LIGHT LENS BROKEN. R & R LENS IAW MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 35,079 hrs · 24,083 cycles

AFT OVERWING EXIT IDENTIFIER B5-120 SIGN INOPERATIVE AT ROW 28. R & R BATTERY CHARGER ASSEMBLY IAW AMM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 35,079 hrs · 24,083 cycles

AFT OVERWING EXIT IDENTIFIER SIGN B5-119 INOPERATIVE AT ROW 28. R & R BATTERY CHARGER ASSEMBLY IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,079 hrs · 24,083 cycles

FORWARD EMER EXIT LIGHT INOPERATIVE. R & R LIGHT ASSEMBLY IAW AMM.

Part: LANYARD — FRAYED (L1 DOOR) · airframe 35,079 hrs · 24,083 cycles

L1 DOOR CONTAINER LANYARD FRAYED. R & R LANYARD IAW AMM.

Part: LENS — CRACKED (EXIT SIGN) · airframe 35,079 hrs · 24,083 cycles

FORWARD OVERWING EXIT SIGN LENS COVERS ABOVE DOORS CRACKED. R & R SIGN IAW AMM.

Part: SUPPORT FITTING — CORRODED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

GALLEY MOUNT SUPPORT FITTING CORRODED AT BS 218, RBL 11. R & R FITTING IAW DWG.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

MAIN CABIN CUSP WEB CRACKED, BETWEEN BS 636 - 655, LBL 60. REPAIRED CUSP WEB IAW SRM.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

MAIN CABIN SEAT TRACK SUPPORT FITTING CRACKED AT BS 737, LBL 44. R & R FITTING IAW DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

MAIN CABIN SUPPORT, SEAT TRACK FITTING CRACKED AT BS 737, RBL 44. R & R FITTING IAW DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

ANGLE CRACKED AT BS 715, RBL 44. R & R ANGLE IAW DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

LEFT SIDE VENT BOX, UPPER AFT ANGLE CRACKED AT BS 1225, LONGERON 5L. R & R ANGLE SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

COPILOTS OTBD SEAT TRACK CORRODED. R & R TRACK IAW DWG. PN OFF 5971207-505, SN OFF N/A, PN ON 5971207-505 & SN ON N/A.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

FRAME VENT BOX VERTICAL ANGLE CRACKED AT BS 200, LT SIDE OTBD. R & R ANGLE IAW DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

FLOOR SUPPORT CORRODED AT BS 180, BETWEEN RBL 20 - 40. R & R SUPPORT IAW DWG.

Part: FORMER — CORRODED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

FORMER CORRODED AT BS 927, BETWEEN LONGERON 29L - 30L. REPAIRED FORMER IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

SHEAR TIE CORRODED AT BS 954, BETWEEN LONGERON 29L - 30L. R & R SHEAR TIE IAW SRM.

Part: MEMBRANE — CORRODED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

MEMBRANE WEB CORRODED AT BS 200, RBL 55. R & R WEB IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

CUSP ANGLE CORRODED AT BS 218, RBL 60. R & R ANGLE IAW EA.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

RIGHT CABIN CUSP WEB CRACKED AT BS 617 RT. REPAIRED CUSP WEB IAW SRM.

Part: FORMER — CRACKED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

FORMER CRACKED AT BS 155, LONGERON 2R. R & R FORMER IAW SRM.

Part: FLOOR SKIN — CORRODED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

MAIN CABIN FLIGHT DECK FLOOR SKIN CORRODED AT BS 145, RBL 16. REPAIRED SKIN IAW EA.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

AFT PIT DOOR, JAMB GUSSET CORRODED, AT BS 994, LONGERON 29R. R & R GUSSET IAW DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

KEEL BEAM FITTING CRACKED AT BS 747, LONGERON 30. R & R FITTING IAW SRM.

Part: FORMER — CORRODED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

WING TO BODY SUPPORT, FORMER CORRODED AT BS 851 LT SIDE LOWER END. REPAIRED FORMER IAW EA.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

SEAT TRACKS CORRODED, BETWEEN BS 274 - 588, RBL 55. R & R SEAT TRACK IAW DWG.

Part: FORMER — CORRODED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

WING TO BODY SUPPORT, FORMER CORRODED AT BS 832, RT SIDE LOWER SECTION. REPAIRED FORMER IAW EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

FORMER CLIP CRACKED AT BS 1022, LONGERON 16R. R & R CLIP IAW DWG.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

LONGERON CORRODED BETWEEN, BS 900 - 1022, LONGERON 30R. R & R LONGERON IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

WING TO BODY SUPPORT ANGLE CRACKED, BETWEEN BS 832 - 842, LONGERON 30. R & R ANGLE IAW DWG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

RIGHT SIDE CUSP WEB, CORRODED AT BS 974, RBL 60. R & R CUSP WEB IAW DWG & SRM.

Part: FORMER — CORRODED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

WING TO BODY SUPPORT FRAME, CORRODED AT BS 832, LT SIDE LOWER SECTION. R & R FORMER IAW DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

SEAT TRACKS CORRODED FROM BS 898 - 1022, RBL 22. R & R SEAT TRACK IAW DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

SEAT TRACKS CORRODED, BETWEEN BS 823 - 898, RBL 22. R & R SEAT TRACK IAW DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

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

Part: FORMER — CORRODED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

WING TO BODY SUPPORT, FORMER CORRODED AT BS 851, RT LOWER END. REPAIRED FORMER IAW EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

LEFT FORMER CLIP CRACKED AT BS 1200, INBD OF VENT BOX. R & R CLIP IAW DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

SEAT TRACKS CORRODED, BETWEEN BS 898 - 1022, RBL 55. R & R SEAT TRACK IAW DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

SEAT TRACKS CORRODED, BETWEEN BS 589 - 898, RBL 55. SEAT TRACK IAW DWG.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

AT CARGO COMPARTMENT, FWD BULKHEAD HORIZONTAL PANEL SUPPORTS CRACKED ALONG THE SUPPORTS. R & R SUPPORTS IAW DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

LEFT CABIN FLOOR WEB SKIN CORRODED AT BS 165, LBL 32. REPAIRED WEB IAW EA.

Part: FITTING — CRACKED (LT MLG WW) · airframe 35,079 hrs · 24,083 cycles

LEFT WW FWD DOOR CUT OUT, INBD FITTING CRACKED. R & R FITTING IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

FORMER CLIP CRACKED AT BS 1152, BETWEEN LONGERON 1L - 2L. R & R CLIP IAW DWG.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

LEFT FWD SIDEWALL PANEL, SUPPORT STRINGER IN FWD CARGO COMPARTMENT, CRACKED AT RIVET FOR PANEL 121AL. R & R SUPPORT IAW DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

MAIN CABIN SEAT TRACK CORRODED, BETWEEN BS 589 - 898, LBL 55. R & R SEAT TRACK IAW SRM & DWG.

Part: FORMER — CRACKED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

RIGHT KEEL BEAM FORMER CRACKED AT BS 679, OTBD END. REPAIRED FORMER IAW EA.

Part: FORMER — CRACKED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

KEEL BEAM AREA FORMER CRACKED AT BS 679, LT OTBD END. R & R FORMER IAW EA.

Part: BONDING STRAP — CRACKED (LT WING) · airframe 35,079 hrs · 24,083 cycles

LEFT WING FIXED LE INBD END, BONDING STRAP CRACKED. R & R STRAP IAW DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

FLOORBOARD SUPPORT CORRODED AT BS 197, BETWEEN LBL 15 - 44.5. R & R SUPPORT IAW DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

MAIN CABIN FWD WET AREA, FLOORBOARD SUPPORT CORRODED, BETWEEN BS 160 - 197, LBL 44.5. R & R SUPPORT IAW DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

L1 DOOR AREA FLOOR SUPPORT CORRODED, BETWEEN BS 165 - 195, LBL 55. R & R SUPPORT IAW DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

MAIN CABIN RT FRAME, CRACKED AT BS 696. R & R FRAME IAW DWG.

Part: FLOOR SKIN — CORRODED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

MAIN CABIN FWD WET AREA, CTR FLOOR SKIN CORRODED AT BS 160, RBL 4. REPAIRED SKIN IAW EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

FLOORBOARD SUPPORT CORRODED, BETWEEN BS 160 - 200, RBL 44. R & R SUPPORT IAW DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

MAIN CABIN FWD WET AREA, FLOOR GALLEY MOUNT CORRODED AT BS 210, RBL 11. R & R SUPPORT IAW DWG.

Part: WEB — CRACKED (R1 DOOR) · airframe 35,079 hrs · 24,083 cycles

R1 DOOR INNER STRUCTURE, WEB CRACKED AT LT SIDE UPPER FRAME. R & R WEB IAW DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

FLOORBOARD SUPPORT CORRODED, BETWEEN BS 200 - 256, LBL 14. R & R SUPPORT IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

FLOORBOARD SUPPORT CORRODED AT BS 220, BETWEEN RBL 8 TO RBL 44. R & R SUPPORT IAW DWG.

Part: TEE FITTING — CRACKED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

T FITTING FOUND CRACKED AT LT DOOR CUT OUT NEAR UPPER LATCH OF THE AFT CABIN EMER DOOR. R & R T FITTING IAW DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 36,622 hrs · 25,128 cycles

RIGHT FRAME CRACKED AT BS 674. R & R FRAME IAW DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

MAIN CABIN SEAT TRACK CORRODED ON UPPER & SIDES OF TRACK, BETWEEN BS 200 - 266, RBL 22. R & R SEAT TRACK IAW DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

MAIN CABIN, FWD WET AREA, FLOORBOARD SUPPORT CORRODED AT BS 148, RBL 12. R & R SUPPORT IAW DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

L2 EMER DOOR CUT OUT AT RT INBD SURFACED ADJACENT TO UPPER DOOR HINGE CRACKED. REPAIRED WEB IAW EA.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

MAIN CABIN SEAT TRACK CORRODED, BETWEEN BS 200 - 245, RBL 44.5. R & R SEAT TRACK IAW DWG.

Part: FLOOR SKIN — CORRODED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

FORWARD WET AREA, FLOOR SKIN CORRODED AT BS 180, RBL 22. REPAIRED SKIN IAW SRM.

Part: FLOOR SKIN — CORRODED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

MAIN CABIN FWD WET AREA, FLOOR SKIN CORRODED AT BS 155, RBL 17. REPAIRED SKIN IAW SRM.

Part: FLOOR SKIN — CORRODED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

FLOOR SKIN CORRODED AT BS 180, RBL 44. R & R SKIN IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

MAIN CABIN FLOORBOARD SUPPORT CORRODED, BETWEEN BS 150 - 200, LBL 5. R & R SUPPORT IAW DWG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

MAIN CABIN CUSP WEB CORRODED, BETWEEN BS 209 - 218, RBL 60. REPAIRED CUSP WEB IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

MAIN CABIN RT FRAME, CRACKED AT BS 674. R & R FRAME IAW DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

FORWARD WET AREA, FLOORBOARD SUPPORT CORRODED, BETWEEN BS 150 - 200, RBL 5. R & R SUPPORT IAW DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

FLOORBOARD SUPPORT CORRODED AT BS 160, BETWEEN RBL 5 TO LBL 5. R & R SUPPORT IAW SRM & DWG.

Part: FLOOR SKIN — CORRODED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

FLOOR SKIN CORRODED AT BS 200, RBL 2. REPAIRED SKIN IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 36,622 hrs · 25,128 cycles

RIGHT FRAME CRACKED AT BS 696. R & R FRAME IAW DWG.

Part: FLOOR SKIN — CORRODED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

FLIGHT DECK FLOOR SKIN CORRODED AT BS 140, BETWEEN BL 0 TO RBL 12. REPAIRED SKIN IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

MAIN CABIN CUSP WEB CORRODED, BETWEEN BS 218 - 237, RBL 60. R & R CUSP WEB IAW DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

FLOORBOARD SUPPORT CORRODED AT BS 200, BETWEEN RBL 5 TO LBL 5. R & R SUPPORT IAW DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

MAIN CABIN WET AREA, FLOORBOARD SUPPORT CORRODED AT BS 237, BL 0. R & R SUPPORT IAW DWG.

Part: FLOOR SKIN — CORRODED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

MAIN CABIN FWD WET AREA, SKIN CORRODED AT BS 160, BETWEEN RBL 17 - RBL 32. REPAIRED SKIN IAW EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

FLOORBOARD SUPPORT CORRODED, BETWEEN BS 160 - 200, RBL 55. R & R SUPPORT IAW DWG.

Part: FLOOR SKIN — CORRODED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

MAIN CABIN FWD WET AREA, FLOOR SKIN CORRODED AT BS 160, BETWEEN RBL 33 - 45. REPAIRED SKIN IAW EA.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

VERTICAL SUPPORT BRACKET CRACKED AT BS 1152, LONGERON 1. R & R BRACKET IAW SRM & DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

R1 DOOR, BETWEEN LOWER & UPPER DOOR HINGES CUT-OUT WEB CRACKED. R & R WEB IAW SRM.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

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

Part: BONDING STRAP — CRACKED (RT WING) · airframe 35,079 hrs · 24,083 cycles

RIGHT WING FIXED LE INBD & BONDING STRAP CRACKED. R & R STRAP IAW DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

WING TO BODY INBD SIDE AT INBD TRACK ANGLE CRACKED. R & R ANGLE IAW DWG.

Part: FITTING — CORRODED (L1 DOOR) · airframe 35,079 hrs · 24,083 cycles

L1 DOOR EMER EVAC SLIDE, FWD GIRT BAR FITTING CORRODED. R & R FITTING IAW AMM.

Part: FITTING — CORRODED (R1 DOOR) · airframe 35,079 hrs · 24,083 cycles

R1 DOOR EMER EVAC SLIDE, AFT GIRT BAR FITTING CORRODED. R & R FITTING IAW AMM.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 35,079 hrs · 24,083 cycles

RIGHT WING SUPPORT T ANGLE CRACKED AT AILERON OTBD HINGE. R & R T ANGLE IAW SRM & DWG.

Part: FITTING — CRACKED (RT WING) · airframe 35,079 hrs · 24,083 cycles

RIGHT WING TO FUSELAGE FITTING, CRACKED AT BS 661, LONGERON 22R. R & R FITTING IAW DWG.

Part: FORMER — CRACKED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

KEEL BEAM AREA FORMER CRACKED AT BS 694, LONGERON 26L. R & R FORMER IAW SRM & DWG.

Part: FORMER — CRACKED (FUSELAGE) · airframe 35,079 hrs · 24,083 cycles

KEEL BEAM AREA, FORMER CRACKED AT BS 694, LONGERON 26R. R & R FORMER IAW DWG.

Part: BATTERY — DISCHARGED (CABIN) · airframe 35,944 hrs · 24,657 cycles

EMERGENCY LIGHTS INOPERATIVE BETWEEN ROW 20 TO 24. R & R BATTERY ASSEMBLY IAW AMM.

Part: GIRT BAR — LOOSE (L1 DOOR) · airframe 35,861 hrs · 24,598 cycles

L1 DOOR EMER EVAC SLIDE GIRT BAR LOOSE. SECURED GIRT BAR IAW MM.

Part: GIRT BAR — LOOSE (R1 DOOR) · airframe 35,861 hrs · 24,598 cycles

R1 DOOR EMER EVAC SLIDE GIRT BAR LOOSE. SECURED GIRT BAR IAW MM.

Part: LANYARD — MISSING (EVAC SLIDE) · airframe 35,868 hrs · 24,603 cycles

R1 DOOR EMER EVAC SLIDE GIRT BAR LANYARD MISSING. INSTALLED LANYARD ASSEMBLY IAW AMM.

Part: GIRT BAR — LOOSE (R1 DOOR) · airframe 35,843 hrs · 24,585 cycles

R1 DOOR EMER EVAC SLIDE GIRT BAR LOOSE. SECURED GIRT BAR IAW AMM.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 34,771 hrs · 23,888 cycles

L1 DOOR SLIDE FELL OUT OF CONTAINER, DID NOT DEPLOY. R & R SLIDE ASSEMBLY IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,621 hrs · 23,793 cycles

R1 DOOR EMERGENCY EXIT SIDEWALL LIGHT INOPERATIVE. R & R LIGHT ASSEMBLY IAW MM.

Part: STIFFENER — CRACKED (RT SPOILER) · airframe 33,950 hrs · 23,361 cycles

RT WING INBD SPOILER OTBD END CRACKED. R & R STIFFENER IAW SRM & DRAWING.

Part: DOUBLER — CRACKED (L1 DOOR) · airframe 33,950 hrs · 23,361 cycles

L1 DOOR NR 1 BEAM DOUBLER CRACKED AT AFT END. R & R DOUBLER IAW SRM.

Part: STRAP — BROKEN (L1 DOOR) · airframe 33,950 hrs · 23,361 cycles

L1 DOOR FWD FRAME LOWER STRAP BROKEN. R & R STRAP IAW SRM & DRAWING.

Part: DOOR — CRACKED (RT WING) · airframe 33,950 hrs · 23,361 cycles

RT WING INBD BUTTE DOOR INBD END CRACKED. REPAIRED DOUBLER IAW EA.

Part: INTERCOSTAL — CRACKED (L1 DOOR) · airframe 33,950 hrs · 23,361 cycles

L1 DOOR FWD FRAME INTERCOSTAL CRACKED. R & R INTERCOSTAL IAW SRM & DRAWING.

Part: LANYARD — WORN (R1 DOOR) · airframe 34,206 hrs · 23,525 cycles

R1 DOOR EMERGENCY EVAC SLIDE CLIP WORN. R & R LANYARD IAW AMM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 34,078 hrs · 23,442 cycles

L1 DOOR EMERGENCY EVAC SLIDE LOOSE. R & R SLIDE IAW MT.

Part: ENGINE — MALFUNCTIONED (RIGHT) · airframe 33,663 hrs · 23,177 cycles

AIR TURN BACK DECLARED EMERGENCY. RT ENGINE COMP STALL ALERT DISPLAYED DURING CLIMB ALONG WITH AUDIBLE SOUNDS & SLIGHT AIRCRAFT YAWING & POWER LOSS. R &R NR 2 ENGINE IAW TC.

Part: GIRT BAR — LOOSE (R1 DOOR) · airframe 33,574 hrs · 23,116 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR LOOSE. SECURED BAR IAW MM.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 32,300 hrs · 22,304 cycles

R1 DOOR EMERGENCY EVAC SLIDE PACK LOOSE. SECURED SLIDE PER AMM.

Part: SLIDE — UNSECURE (R1 DOOR) · airframe 31,847 hrs · 22,006 cycles

R-1 SLIDE PAC UNSECURE. RE-SECURED R-1 SLIDE LOCK PER MM 25-61-03. OK FOR SERVICE.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 31,836 hrs · 21,998 cycles

R1 DOOR SLIDE OUT OF GREEN ON LOW SIDE. REMOVED AND REPLACED R1 DOOR SLIDE REF AMM.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 21,999 hrs · 21,998 cycles

R-1 DOOR SLIDE OUT OF GREEN ON LOW SIDE. REMOVED AND REPLACED R1 DOOR SLIDE REF AMMJ 25-61-03.

Part: BATTERY — DISCHARGED (CABIN) · airframe 29,829 hrs · 20,702 cycles

EMERGENCY LIGHT INOP BETWEEN ROW 1 TO ROW 3. REMOVED AND REPLACED BATTERY PER AMM.

Part: CABLE — LOOSE (EVAC SLIDE) · airframe 29,227 hrs · 20,315 cycles

R1 DOOR EMERGENCY EVAC SLIDE CABLE LOOSE. SECURED CABLE PER MM.

Part: STRINGER — CORRODED (FUSELAGE)

AFT PIT BILGE AREA STRINGER, STA 927 TO 986, LONG 30, CORROSION. ACCOMPLISHED STRINGER FILLER AND SPLICE REPAIR PER B71 SRM 53-00-05. SEE NR 21508.

Part: DOOR FRAME — CORRODED (FUSELAGE)

FWD CARGO DOOR LOWER JAMB, STA 370 TO 427, CORROSION. ACCOMPLISHED LOWER JAMB REAPAIR PER B717 SRM 53-20-15. SEE NR 21499 AND 21565.

Part: PAN — CRACKED (CARGO BAY)

FWD CARGO COMPARTMENT FWD DOOR PAN, CRACKED. ACCOMPLISHED FWD DOOR PAN REPLACEMENT PER B717 SRM 52-30-02, 51-10-04.

Part: PAN — CRACKED (CARGO BAY)

FWD CARGO COMPARTMENT AFT DOOR PAN, CRACKED. ACCOMPLISHED AFT DOOR PAN REPLACEMENT PER B717 SRM 52-30-02, 51-10-04.

Part: SPLICE — CORRODED (CARGO BAY)

AFT CARGO COMPARTMENT LOWER DOOR JAMB SEAL DEPRESSOR SPLICES, CORROSION. ACCOMPLISHED LOWER DOOR JAMB SEAL DEPRESSOR SPLICES REPLACEMENT PER B717 SRM 51-20-09, 51-40-08.

Part: LIGHT — DEFECTIVE (CABIN)

EMERGENCY LIGHT ASSEMBLY AT SEAT 15D NEEDS TO BE REPLACED. REMOVED AND REPLACED BAD EMERGENCY LIGHT ASSY AT SEAT 15D. REF AMM 33-51, OPS CHECK GOOD.

Part: COVER — MISSING (CABIN)

THE 21D EXIT ROW SEAT RED CAP COVER AT BASE OF SEAT IS MISSING. INSTALLED MISSING SEAT 21D EXIT ROW RED LENS COVER.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

CEILING EMERGENCY LIGHTS ABOVE ROWS 29/30 INOP. REMOVED AND REPLACED BATTERY POWER SUPPLY & PERFORMED OPS TEST, OPS TEST WAS NORMAL REF 33-51-03 B717 MM.

Part: WIRE — BROKEN (CABIN)

E-PATH LIGHTS AT SEAT ROW 10DEF (2 ASSY) INOP. REPAIRED BROKEN WIRING AT SEAT DISCONNECT IAW SWPM 20-31-17 & SWPM 20-10-01. OPS CHECK NORMAL RE AMM 33-51-00.

Part: LIGHT — INOPERATIVE (CABIN)

SEAT 19 D EMERGENCY ESCAPE PATH LIGHT INOP. RELAMPED 19D EMERGENCY ESCAPE PATH LIGHT OPS CHECK GOOD MM REF 33 51 00.

Part: LIGHT — INOPERATIVE (CABIN)

THE10D ESCAPE LIGHT INOP. REPLACED 10D EMERGENCY PATH LIGHT LENS AND BULB.

Part: LIGHT — INOPERATIVE (CABIN)

THE 10D ONE E PATH BULB INOP. REPLACED BURNED OUT EPL BULB AT LOCATION 10D. PERFORMED OPS CHECK OF EPL LIGHTING PER MM 33-51-00. THIS CLEARS MDDR 205214.

Part: LIGHT — INOPERATIVE (CABIN)

SEAT ROWS 25-31 EMERGENCY LIGHTS INOP.

Part: ELECTRICAL SYS — SATURATED (COCKPIT)

NUMEROUS ELECTRICAL FAILURES, STATUS PAGE REVEALED MULTIPLE ALERT FAILURES. DURING INITIAL EVALUATION FOUND WATER AT F/O'S SLIDING WINDOW LOWER CONSOLE AREA. WHEN EBAY DOOR OPENED LARGE AMOUNT OF WATER CAME OUT. INSPECTED AND DRIED F/O'S CONSOLE AREA, UNDER F/O'S FLOORBOARD, ALL E&E BAY AREAS AND INSULATION BLANKETS. REMOVED AND REPLACED EPCU, PA AMP, FCC NR 2, VIA NR 2, PODS, VHF NR 1, VHF NR 3, REU, PCDU-R, BATTERY RELAY AND APU START RELAY DUE TO WATER DAMAGE. REF N/R N081817 FOR ALL OPS CHECKS AND RTS.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

EMERGENCY LIGHTS ARE OUT AT SEATS ROWS 1, 2, 3 AND 10. ALSO BETWEEN THE FWD LAV AND G2 GALLEY. REPLACED BATTERY SUPPLY ASSY ABOVE SEAT 3DF OPS CHECK NORMAL REF 33-51.

Part: ENGINE — FAILED (NR 2)

RIGHT ENGINE FAILED DURING CLIMBOUT APPROX 3-5 MINUTES AFTER TAKEOFF, R- TGT GOT TO APPROX 1100 DEG C; R- N-2 WENT TO 0 AFTER APPROX 1 MIN FOLLOWING FAILURE. REMOVED AND REPLACED NR 2 ENGINE ASSY IAW TASK CARD 603; OPS CHECK GOOD AND LEAK CHECK GOOD.

Part: CONNECTOR — DEFECTIVE (CABIN)

WORKING TECH SUPPORT REQUEST- EMERGENCY LIGHTS INOPERATIVE SEAT ROW 25-31. FOUND CONNECTOR AT SEAT 25 WITH ONE PIN PUSHED BACK, AND BATTERY PACK FUSE SHORTED. REPLACED CONNECTOR PER B717 SWPM 20-31-00 AND REPLACED BATTERY PACK PER B717 AMM 33-51-03. OPS CHECK GOOD PER B717 AMM 33-51-00.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

DURING SVC EMERGENCY LIGHTS AT SEAT 25-31 INOP. REPLACED BATTERY SUPPLY ASSY AT B5-119 IAW AMM 33-51. OK FOR SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

EMERGENCY LIGHTS INOPERATIVE AT ROWS 25 TO 31. REPLACED BATTERY SUPPLY ASSY AT B5-119 IAW AMM 33-51, CHECKS OK.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

EMERGENCY LIGHTS AT SEATS 25-31 INOPERATIVE. REMOVED AND REPLACED B5-119 BATTERY SUPPLY ASSEMBLY REF AMM 33-51.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

WHILE PERFORMING SERVICE CHECK, FOUND ROWS 24-31 EMERGENCY PATH LIGHTS INOP. REMOVED AND REPLACED B5-119 EMERGENCY LIGHT POWER SUPPLY IAW MM 33-51. OPS CHECK OK.

Part: PAN — CORRODED (FUSELAGE)

ABOVE WASTE COMPARTMENT, GALLEY 2 PAN, CORROSION. ACCOMPLISHED GALLEY 2 PAN REPLACEMENT PER B717 SRM 51-41-02.

Part: SUPPORT — CORRODED (FUSELAGE)

RIGHT AFT WING TO BODY SUPPORT STRAP, STA 832, CORROSION. ACCOMPLISHED WING TO BODY SUPPORT STRAP REPLACEMENT PER B717 SRM 51-41-02.

Part: SKIN — CORRODED (FUSELAGE)

AFT FUSELAGE SKIN, STA 851 TO 861, LBL 6 TO RBL 6, CORROSION. ACCOMPLISHED FUSELAGE SKIN DOUBLER REPAIR PER EA 17-53-02452IR.

Part: FITTING — CRACKED (RT MLG DOOR)

RIGHT MLG DOOR, FWD OF UPLOCK ROLLER FITTING CRACKED. ACCOMPLISHED DOUBLER REPAIR PER TRA 17-52-TR00134.

Part: SEAT TRACK — CORRODED (FUSELAGE)

CABIN SEAT TRACK, STA 200 TO 266, RBL 22, CORROSION. ACCOMPLISHED SEAT TRACK SPLICE REPAIR PER DC9 SRM 53-05 FIG 4F.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT BEAM, STA 160 TO 200, RBL 44, CORROSION. ACCOMPLISHED FLOOR SUPPORT BEAM REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT BEAM, STA 165 TO 200, LBL 8, CORROSION. ACCOMPLISHED FLOOR SUPPORT BEAM REPLACEMENT PER B717 SRM 51-41-05.

Part: WEB — CORRODED (FUSELAGE)

CABIN FLOOR WEB, STA 200 TO 218, RBL 54, CORROSION. ACCOMPLISHED FLOOR WEB DOUBLER REPAIR PER B717 SRM 51-70-10 FIG 201 REPAIR 1.

Part: BRACKET — CORRODED (FUSELAGE)

CABIN FLOOR WEB, STA 165 TO 200, LBL 10 TO RBL 10, CORROSION. ACCOMPLISHED FLOOR WEB DOUBLER AND SPLICE REPAIR PER B717 SRM 51-70-10 FIG 201 REPAIR 2.

Part: BRACKET — CORRODED (FUSELAGE)

CABIN FLOOR WEB BRACKET, STA 541 TO 560, LONG L18R, CORROSION. ACCOMPLISHED FLOOR WEB BRACKET REPLACEMENT PER B717 SRM 51-41-02.

Part: STRAP — CORRODED (FUSELAGE)

AFT EXTERIOR WING TO BODY SUPPORT STRAP, STA 832, BL 0, CORROSION. ACCOMPLISHED EXTERIOR WING TO BODY SUPPORT STRAP REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT BEAM, STA 180, RBL 6 TO RBL 40, CORROSION. ACCOMPLISHED FLOOR SUPPORT BEAM REPLACEMENT PER B717 SRM 51-41-02 AND B717 SRM 51-41-05.

Part: FLOORBEAM — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT BEAM, STA 160, LBL 6 TO RBL 6, CORROSION. ACCOMPLISHED FLOOR SUPPORT BEAM REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT BEAM, STA 165 TO 200, RBL 6, CORROSION. ACCOMPLISHED FLOOR SUPPORT BEAM REPLACEMENT PER B717 SRM 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT BEAM, STA 200, LBL 12, CORROSION. ACCOMPLISHED FLOOR SUPPORT BEAM REPLACEMENT PER B717 SRM 51-41-02.

Part: SEAT TRACK — CORRODED (FUSELAGE)

CABIN SEAT TRACK, STA 200 TO 247, RBL 44.5, CORROSION. ACCOMPLISHED SEAT TRACK SPLICE REPAIR PER DC9 SRM 53-05 FIG 4F AND EA 17-53-02456IR.

Part: FLOORBEAM — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT BEAM, STA 200, LBL 6 TO RBL 6, CORROSION. ACCOMPLISHED FLOOR SUPPORT BEAM REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

GALLEY ENTRANCE FLOOR SUPPORT BEAM, CORROSION. ACCOMPLISHED FLOOR SUPPORT BEAM REPLACEMENT PER B717 SRM 51-41-02.

Part: SPLICE PLATE — CORRODED (FUSELAGE)

LEFT WING TO BODY FAIRING SPLICE PLATE, STA 851, CORROSION. ACCOMPLISHED SPLICE PLATE REPLACEMENT PER B717 SRM 51-41-01.

Part: FLOORBEAM — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT BEAM, STA 200, RBL 8 TO RBL 48, CORROSION. ACCOMPLISHED FLOOR SUPPORT BEAM REPLACEMENT PER B717 SRM 51-41-02.

Part: SPLICE PLATE — CORRODED (FUSELAGE)

RIGHT WING TO BODY FAIRING SPLICE PLATE, STA 851, CORROSION. ACCOMPLISHED SPLICE PLATE REPLACEMENT PER B717 SRM 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT BEAM, STA 237, BL 0, CORROSION. ACCOMPLISHED FLOOR SUPPORT BEAM REPLACEMENT PER B717 SRM 51-41-02.

Part: FLOORBEAM — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT BEAM, STA 150, RBL 32 TO RBL 45, CORROSION. ACCOMPLISHED FLOOR SUPPORT BEAM REPLACEMENT PER B717 SRM 51-41-02.

Part: PIN — BROKEN (CONNECTOR)

EMERGENCY LIGHTS INOPERATIVE AT ROW 16 DEF. RE-TERMINATED EMERGENCY LIGHT CONNECTOR AT 16 RT IAW RES 02-1008. EMERGENCY LIGHTS CHECK OK IAW MM 33-51.

Part: PAN — CORRODED (FUSELAGE)

AFT CARGO DOOR JAMB LOWER PAN CORROSION. CUT OUT CORRODED AREA, REPLACED PAN AND SPLICES IAW B717 SRM 53-20-15.

Part: LANYARD — BROKEN (L1 DOOR SLIDE)

ESCAPE SLIDE AT L-1 DOOR WIRE LANYARD BROKEN. R&R WIRE LANYARD IAW REF MM 25-61

Part: CHARGER — INOPERATIVE (CABIN)

EMERGENCY PATH LIGHTING AT SEATS 1DF, 2DF & 3DF WOULD NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY PATH LIGHTING BATTERY CHARGER AT LOCATION 222AR, REF AMM 33-51.

Part: POWER SUPPLY — DISCHARGED (CABIN)

EMERGENCY BATTERY SUPPLY STA 332 INOPERATIVE. REPLACED EMERGENCY BATTERY SUPPLY PER MM 33-50. OPS CHECK GOOD.

Part: SKIN — DAMAGED (BS 1087 L10L)

FOUND HOLE IN FUSELAGE UNPRESSURIZED AREA AT STATION 1087 LONGERON 10L HOLE SIZE 5 IN X 1.5. REPAIRED FUSELAGE AT STA 1087 LONGERON 10 L REF AAR W/O 28330 PER SRM 53-00-00 REPAIR 2.

Part: BATTERY PACK — UNSERVICEABLE (EMERGENCY LIGHT)

FIRST CLASS EMERGENCY LIGHTS WILL NOT TEST. REMOVED AND REPLACED B5-118 BATTERY AND BATTERY SUPPLY ASSY REF AMM 33-51.

Part: POWER SUPPLY — DISCHARGED (CABIN)

EPL LIGHTING IS OUT FROM SEATS 1D - 10D. REMOVED AND REPLACED BATTER PACK POWER SUPPLY ASSY B5-118. OPS CHECK GOOD REF AMM 33-51.

Part: SKIN — DENTED (FUSELAGE)

MAJOR REPAIR TO FUS STA 237 LONG 16 AND 17 LT SIDE DENTED. FABRICATED DOUBLER REPAIR PER B717 SRM 53-00-01 REPAIR 6.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY LIGHTS AT SEAT 11-19 INOPERATIVE. EMERGENCY LIGHT BATTERY SUPPLY ASSY WAS REMOVED AND REPLACED AS PER AMM 33-51. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN)

ROWS 1, 2, 3, 10 EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED NR 4 BATTERY SUPPY PACK IAW MM 33-51.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY LIGHTS AT R-1 DOOR INOP (CEILING). REMOVED AND REPLACED EMERGENCY LIGHT BATTERY SUPPLY ASSEMBLY. OPS CHECKED NORMAL. REF AMM 33-51.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY ROW LIGHTS ON SEATS 1AC, 2AC AND 3AC INOPERATIVE. REMOVED & REPLACED POWER SUPPLY ASSYS AT STA 341 B5-118 & STA 213, B5-235 REF 33-51 M/M.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SERVICE CHECK FOUND ROWS 1-10 EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY SUPPLY ASSY.