N977AT

Part: NOT REPORTED — NOT REPORTED (ZONE 300) · airframe 59,917 hrs · 42,766 cycles

ER/A 628422-14AD REVISION ORIGINAL. REPAIR AT LT SIDE OF VERTICAL STAB SPAR AT ZFS=52.267. (1144341)

Part: SKIN — CRACKED (ZONE 300) · airframe 59,896 hrs · 42,747 cycles

SHIP 9541 C/W ERA 628422-14AD REV ORIG VERTICAL STABILIZER LHS & RHS LEADING EDGE SKIN ZFS52.267 FASTENER HOLES CRACKED. CORRECTIVE ACTION: C/W PRI 628422-14AD. (1145072)

Part: FITTING — DAMAGED (ZONE 500) · airframe 59,506 hrs · 42,389 cycles

AIRCRAFT 9541, LEFT WING LOWER SURFACE BRACE FITTING AT STA XRS 164 HOLE HAS DAMAGE (1EA) LABLED C1. CORRECTIVE ACTION: LEFT WING LOWER SERFACE BRACE FITTING STA XR5164, REAMED HOLE C1.416 IAW ER/A 623679-14 AD REV 0 PRI REV 4 PERFORMED BHEC INSP IAW ERS 623679-14 AD REV 0. NO CRACKS NOTED.REPLACED DAMAGED BRACE FITTING AT LEFT WING LOWER SURFACE PER ERA623679-14AD REV. ORIGINAL. (LP 1007416)

Part: SPAR — DAMAGED (ZONE 500) · airframe 59,505 hrs · 42,388 cycles

SHIP 9451 LH WING AFT SPAR FLAP TRACK MOUNT REQUIRES REMOVAL OF 8 BUSHINGS TO FOM SPAR REPAIR. CORRECTIVE ACTION: REPAIRED PER 623679-14AD REV 0 (0996171)

Part: SKIN — DAMAGED (ZONE 500) · airframe 59,505 hrs · 42,388 cycles

SHIP 9541 LEFT WING LOWER SURFACE AFT SPAR HOLES HAVE DAMAGE FROM STA XRS 111 TO XRS 137. CORRECTIVE ACTION: DAMAGE WAS REMOVED IAW DELTA ER/A 623679-14AD (0982505)

Part: SPAR CAP — CRACKED (ZONE 600) · airframe 59,505 hrs · 42,388 cycles

SHIP 9541 B717-200 / RH WING / REAR SPAR / LOWER CAP / XRS=164 / CRACK. CORRECTIVE ACTION: ASSOCIATED ER/A 00-623681 C/W. (0980036)

Part: SPAR WEB — DAMAGED (ZONE 500) · airframe 59,505 hrs · 42,388 cycles

LEFT WING AFT SPAR WEB O/B LOWER HOLE HAS DAMAGE (1 EA), LABELED AS B1. NO DAMAGE FOUND IAW DELTA ER/A 623679-14AD REV 0, PRI REV 7 SECTION 4 STEP #1 AND TABLE 2. ASSOCIATED ER/A 14-623679 ADDED FOR AC 9541. (LP #0941455)

Part: SKIN — DAMAGED (ZONE 500) · airframe 59,505 hrs · 42,388 cycles

LEFT WING LOWER SURFACE AFT SPAR HOLES HAVE DAMAGE FROM STA XRS 111 TO XRS 137 (7 EA) MARKED AS A1 THRU A7. DAMAGE WAS REMOVED IAW DELTA ER/A 623679-14AD REV 0 PRI REV 7 SECTION IV STEP # 5, #6, AND #7. ASSOCIATED ER/A 14-623679 ADDED FOR AC 9541. (LP #0941448)

Part: SPAR CAP — CRACKED (ZONE 500) · airframe 59,498 hrs · 42,378 cycles

-AD- CRACKS FOUND DURING INSPECTION OF LH WING REAR SPAR LOWER CAP RADIUS. CONTACT LIASON ENGINEERING FOR REPAIR PROCEDURES PRIOR TO FURTHER FLIGHT REF FC5720-01103. CRACK IS LOCATED INBD OF XRS 164 AT RIVET HEAD 1/2 INCH ABOVE LWR RADIUS. DISCREPANCY TRANSFERRED TO NR#5 OF WORK PACKAGE 5625764. C/W ERA 615810-14AD REV E PRI REV 5. PRI AND ERA MATCH. (LP #6750154)

Part: SPAR — CRACKED (ZONE 500) · airframe 59,362 hrs · 42,260 cycles

-AD- WORKING PRI 615810-14AD REV 0. LH WING SPAR CRACK FUEL LEAK. ACCOMPLISHED PRI 615810-14AD REVISION D, REV 3. VERIFIED ERA 615810-14AD REV D SECTION VI TIME LIMITED REPAIR III MATCHES COMPLETED PRI 615810-14AD REV 0, 1, 2, AND 3. ASSOCIATED ER/A 14-615810 ADDED FOR AC 9541. (LP #0679762)

Part: NONE — NONE (NONE) · airframe 59,236 hrs · 42,144 cycles

-AD- WORKING PRI 615810AD REV 3. C/W ALL STEPS OF ERA 615810-14AD REV A SECTION IV TIME LIMITED REPAIR II. THESE STEPS ARE C/W AND MATCH PRI 621847-14AD REV 0, 1, 2, AND PRI 615810-14AD REV 3. (LP #0634418)

Part: FUEL CELL — LEAKING (ZONE 500) · airframe 59,236 hrs · 42,144 cycles

-AD- L/H WING REAR SPAR LOWER CAP LEAKING FUEL. C/W PRI 621847-14AD REV 2. C/W ALL STEPS OF ERA 615810-14AD REV A SECTION IV TIME LIMITED REPAIR II. THESE STEPS MATCH PRI 621847-14AD REV 0, 1, 2, AND PRI 615810 REV 3. (LP #0634404)

Part: FUEL CELL — LEAKING (ZONE 500) · airframe 59,236 hrs · 42,144 cycles

-AD- FUEL LEAK FOUND DURING INSPECTION OF THE LH WING REAR SPAR LOWER CAP. CONTACT LIAISON ENG. REPAIR PROCEDURES PRIOR TO FURTHER FLIGHT, AA#FC5720-01103. LEAK IDENTIFIED ORIGINATED FROM FASTENER. C/W PRI 621847-14AD REV ORIGINAL THRU REV 2. C/W PRI 615810-14AD REV 3. PERFORMED LEAK CHECK NO FURTHER LEAKS. C/W ALL STEPS OF ERA 615810-14AD REV A SECTION IV TIME LIMITED REPAIR II. (LP #0634390)

Part: SPAR — CRACKED (ZONE 500) · airframe 59,360 hrs · 42,257 cycles

-AD- LH WING REAR SPAR XRS 164 CRACKED. ADDITIONAL ENGINEERING AUTHORIZATION (ER/A REVISION) REQUIRED FOR CONTINUED SERVICE BEYOND 06NOV2024 (AD EFFECTIVE DATE). A NEW FAA FORM 8100-9 AND AMOC APPROVAL TO AD 2024-21-01 IS REQUIRED FOR CONTINUED SERVICE BEYOND THIS LIMIT. ASSOCIATED ER/A 14-615810 ADDED FOR AC 9541. ER/A 615810-14 IS CURRENTLY AT REVISION B. THE AMOC TRACKING TIME LIMIT IS CHANGED FROM 06NOV24 TO 22NOV24. ADDITIONAL ENGINEERING AUTHORIZATION (ER/A REVISION) REQUIRED FOR CONTINUED SERVICE BEYOND 22NOV24. A NEW FAA FORM 8100-9 AND AMOC APPROVAL TO AD 2024-21-01 IS REQUIRED FOR CONTINUED SERVICE BEYOND THIS LIMIT. ER/A 615810-14AD IS CURRENTLY AT REVISION C. AMOC TO AD 2024-21-01 APPROVAL RECEIVED AND INCORPORATED IN ER/A 615810-14AD REVISION C. CLOSED LOG AND REMOVED MONITOR INSP PER ALERT 18NOV24 AND LOG COMMENTS. (LP #0631778)

Part: LENS — MISSING (ZONE 200) · airframe 59,079 hrs · 42,017 cycles

THE 1AB EMERGENCY LIGHT LENSE IS MISSING. MAINTENANCE REPLACED THE EMERGENCY LIGHT COVER AT 1AB AS REQUIRED. OK FOR SERVICE. (LP #0569847)

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 58,681 hrs · 41,656 cycles

DURING THE SERVICE CHECK, THE TAIL SIDE EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE FOUND THE BATTERY PACK (B5-260) DEFECTIVE. THE BATTERY PACK WAS REPLACED PER B717 AMM 33-51. OPERATIONAL CHECK IS NOW GOOD. (LP #5916991)

Part: LANYARD — MISSING (DOOR SLIDE) · airframe 58,133 hrs · 41,202 cycles

SLIDE DISARMING PIN ATTACHING LANYARD MISSING. LATCH MECHANISM MISSING TO SECURELY ARM TAILCONE. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. WILL REQUIRE NEW LOWER CATCH ASSY AND ATTACHING HARDWARE FOR APU DOOR ARMING LEVER COVER PER B717 IPC 25-23-03 ITEMS 64-83. NASI EWR. FWD TO NEF 52-12-01. PLEASE SEE LOG #5535162 FOR CORRECTIVE ACTION. (LP #0295798)

Part: DOOR FRAME — DAMAGED · airframe 58,074 hrs · 41,153 cycles

CRACK DOOR ON FRAME DOOR ANGLE BTW STA 195 (AFT UPPER CORNER) AT FWD SERVICE DOOR R1. SUMMARY OF NRC 00075: ANGLE WAS FABRICATED PER DOUGLAS AIRCRAFT COMPANY DRAWING: 9911579 REV: L AND REPLACED PER B717-200 SRM 51-41-05-0G. (LP #0279803)

Part: BEAM — DAMAGED · airframe 58,074 hrs · 41,153 cycles

CRACK BEYOND STOPDRILL, (PREVIOUS REPAIR) ON DOOR BEAM 1 BTW STA 190-200 (UPPER AFT CORNER) AT FWD PASSENGER DOOR L1. SUMMARY OF NRC 00071: DOOR BEAM 1 BTW STA 190-200 (UPPER AFT CORNER) AT FWD PASSENGER DOOR L1 WAS REPAIRED PER B717-200 SRM 52-10-02-2R, PROCEDURE 7, FIGURE 201. (LP #0279502)

Part: SPAR — CRACKED (LT WING) · airframe 58,073 hrs · 41,152 cycles

CRACK ON REAR SPAR XRS 150 AT LH WING. SUMMARY OF NRC 0054: REAR SPAR XRS 150 AT LH WING WAS REPAIRED PER ERA 615810-14 REV ORIGINAL SECTION I: TEMPORARY REPAIR. TIME CONTROLLED ITEMS, SEC II ACCOMPLISH SECTION II: INITIAL HFEC SURFACE INSPECTION AND DVI PRIOR TO 41,452 TOTAL FLIGHT CYCLES (300 FLIGHT CYCLES FROM ERA ISSUANCE) AND THEN REPETITIVELY EVERY 400 FLIGHT CYCLES THEREAFTER. MONITORED WITH LP 0274423. SEC III ACCOMPLISH SECTION III: PERMANENT REPAIR PRIOR TO 42,652 TOTAL FLIGHT CYCLES (1500 FLIGHT CYCLES FROM ERA ISSUANCE). MONITORED WITH LP 0274423. (LP #0277849)

Part: PAN — CRACKED (FWD CARGO) · airframe 58,073 hrs · 41,152 cycles

CRACK PAN ON AFT EDGE AT FWD CARGO COMPARMENT DOOR. SUMMARY OF NRC 00154: FWD CARGO COMPARMENT DOOR WAS REPAIRED PER ERA 559551-14 REV A. SECTION II. ASSOCIATED ER/A 14-559551 ADDED FOR AC 9541. (LP #0263823)

Part: SKIN — DEBONDED (LT TE FLAP VANE) · airframe 58,073 hrs · 41,152 cycles

TWO DISBONDS FOUND ON LH AFT MOVABLE FLAP VANE LOWER SKIN: 1) LENGTH=1.700IN, WIDTH=1.500IN AND 2) LENGTH=2.100IN, WIDTH= 1.000IN (IN REF MON/9541/0138992 JOB # 005-0001). SUMMARY OF NRC 00037: LH AFT MOVABLE FLAP VANE LOWER SKIN WAS REPAIRED PER ERA 595913-14 REV A SECTION II: PERMANENT REPAIR AND PRI 595913-14 REV 1. ASSOCIATED ERA 14-595913 ADDED FOR AC 9541. (LP #0260220)

Part: PAN — CRACKED (FWD CARGO) · airframe 58,073 hrs · 41,152 cycles

CRACK ON PAN FWD UPPER CORNER AT FWD CARGO COMPARMENT DOOR. SUMMARY OF NRC 00155: PAN FWD UPPER CORNER AT FWD CARGO COMPARMENT DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R REPAIR 1. (LP #0257725)

Part: WINDOW FRAME — CRACKED (SLIDING WINDOW) · airframe 58,073 hrs · 41,152 cycles

CRACK ON UPPER AFT CORNER CUTOUT OF LH SLIDING WINDOW, AT COCKPIT. SUMMARY OF NRC 00439: UPPER AFT CORNER CUTOUT OF LH SLIDING WINDOW AT COCKPIT WAS REPAIRED PER B717-200 SRM 56-10-02-2R PROCEDURE 1 REPAIR 1. BRACKET OF UPPER AFT CORNER CUTOUT OF LH SLIDING WINDOW WAS REPLACED PER B717 SRM 51-41-01-0G, 51-41 -05-0G, AND 51-41-02-0G. PERFORM VISUAL INSPECTION EVERY "C" CHECK PER B 717 SRM 56-10-02-2R PROCEDURE 1, STEP 6. DFRD BY MON INSP 00000029 ATL 21MAR24 RII: Y ENTR 00165638 S **REDEFERRED LOG TO QC, ESTAB MON INSP **00-0556-8-6420 S/N 09541 REP. (LP #0254620)

Part: CUSP WEB — CORRODED (BS 148-218) · corrosion level 2 · airframe 58,073 hrs · 41,152 cycles

CORROSION ON RH CUSP ANGLE BTW STA Y=148 TO Y=218. SUMMARY OF NRC 00438: CORROSION LEVEL 2. RH CUSP ANGLE BTW STA Y=148 TO Y=218 WAS REPAIRED PER ERA 616020-14 REV ORIGINAL. SECTION I: PERMANENT REPAIR. ASSOCIATED ERA 14-616020 ADDED FOR AC 9541. (LP #0251319)

Part: FLOOR SUPPORT — CORRODED (BS 160-200) · corrosion level 2 · airframe 58,073 hrs · 41,152 cycles

CORROSION ON FLOOR SUPPORT BTW STA Y=160-200 X=6, X=0 AND X=-6. SUMMARY OF NRC 00620: CORROSION LEVEL 2. FLOOR SUPPORTS BTW STA Y=160-200 X=6, X=0 AND X=-6 WERE REPLACED PER B717-200 SRM 51-41-01-0G, 51-41-02-0G, AND 51-41-05-0G. (LP #0246907)

Part: ANGLE — CORRODED (FRM 1087 L18R) · corrosion level 2 · airframe 58,073 hrs · 41,152 cycles

CORROSION ON FRAME CLIP STA Y=1087 AND LONGERON 18R AT AFT ACCESORY COMPARTMENT. SUMMARY OF NRC 00101: CORROSION LEVEL 2. FRAME CLIP STA Y=1087 AND LONGERON 18R AT AFT ACCESORY COMPARTMENT WAS FABRICATED PER B717 DWG S2931622 REV B AND REPLACED PER B717 SRM 51-41-02-0G AND 51-41-05-0G. (LP #0245630)

Part: SEAT TRACK — CORRODED (BS 200-256) · corrosion level 2 · airframe 58,073 hrs · 41,152 cycles

CORROSION ON SEAT TRACK BTW Y=200 TO STA Y=256, COORDINATE X=-44 (RH SIDE). SUMMARY OF NRC 00696: CORROSION LEVEL 2. SEAT TRACK BTW Y=200 TO STA Y=341, COORDINATE X=-44 (RH SIDE) WAS FABRICATED PER DRAWING #5930547 REV CW AND REPLACED PER B717 SRM 51-41-01-0G, 51-41-05-0G, AND 51-41-02-0G. (LP #0242349)

Part: CUSP WEB — CORRODED (BS 446-465) · corrosion level 2 · airframe 58,073 hrs · 41,152 cycles

CORROSION ON RH CUSP WEB LOWER SURFACES BTW STA 446 TO STA 465 AND STA 494 TO STA 500. SUMMARY OF NRC 00669: CORROSION LEVEL 2. RH CUSP WEBS BTW STA 446 TO STA 465 AND STA 494 TO STA 500 WERE REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #0242247)

Part: PAN — CRACKED (DOOR AREA) · airframe 58,073 hrs · 41,152 cycles

CRACK ON DOOR PAN AFT UPPER CORNER AT FWD PASSENGER DOOR. SUMMARY OF NRC 00119: DOOR PAN AFT UPPER CORNER AT FWD PASSENGER DOOR WAS REPAIRED PER B717-200 SRM 52-10-02-2R REPAIR 3. (LP #0234310)

Part: WEB — CORRODED (BS 200-205) · corrosion level 2 · airframe 58,073 hrs · 41,152 cycles

CORROSION ON WEB BTW STA Y=200/205 AND STA X=54 AT C PAX (W1) WAS FOUND OUT OF LIMITS. SUMMARY OF NRC 00719: CORROSION LEVEL 2. WEB BTW STA Y=200/205 AND STA X=54 AT C PAX WAS REPAIRED PER B717 SRM 51-70-10-2R REPAIR 2. (LP #0233534)

Part: CUSP WEB — CORRODED (BS 655-715) · airframe 58,073 hrs · 41,152 cycles

AWR, AA, AD IN REF TO AMDS 5310-01436-03B STEP 3: AFTER RH CUSP WEB REMOVAL, SEVERAL CRACKS AND CORROSION WERE FOUND ON RIGHT CUSP WEB FROM STA Y 655 TO 715. SUMMARY OF NRC 00700: RH CUSP WEB FROM STA Y 655 TO 715 WAS REPAIRED PER B717 SRM 53-00-55-2R-4. ASSOCIATED AA 5310-01436 ADDED FOR AC 9541. (LP #0233487)

Part: LONGERON — CORRODED · corrosion level 2 · airframe 58,073 hrs · 41,152 cycles

CORROSION WAS FOUND OUT OF LIMITS AT LONGERON ENDS 28LH AND 28RH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00713: CORROSION LEVEL 2. LONGERON ENDS 28LH AND 28RH WERE DRILLED AND ADJUSTED PER B717 SRM 51-40-08-0G AND REPLACED UNDER NRC 00464 AND PER B717 SRM 51-41-05-0G. (LP #0233143)

Part: FRAME — CRACKED (BS 1037 L17L) · airframe 58,073 hrs · 41,152 cycles

CRACK ON FRAME STA=1037 LONGERON 17LH SIDE AT PAX CABIN. SUMMARY OF NRC 00411: FRAME STA=1037 LONGERON 17LH SIDE AT PAX CABIN WAS REPAIRED PER B717 SRM 53-20-07-2R AND 51-41-05-0G. (LP #0231352)

Part: FLOOR SUPPORT — CORRODED (BS 200-218) · corrosion level 2 · airframe 58,073 hrs · 41,152 cycles

CORROSION ON FLOOR SUPOORT BTW STA Y=200 TO 218 X-54 AT PAX CABIN. SUMMARY OF NRC 00708: CORROSION LEVEL 2. FLOOR SUPPORT BTW STA Y=200 TO 218 X-54 WAS FABRICATED PER DWG 5952262 REV L AND REPLACED UNDER NRC 00438. (LP #0230263)

Part: CUSP WEB — CORRODED (BS 484-494) · corrosion level 2 · airframe 58,073 hrs · 41,152 cycles

CORROSION ON RH CUSP WEB REPAIR DOUBLER BTW STA 484 TO 494 PAX CABIN. SUMMARY OF NRC 00484: CORROSION LEVEL 2. RH CUSP WEB REPAIR DOUBLER AND RING DOUBLER BTW STA 484 TO 494 PAX CABIN WERE REPLACED PER B717 SRM 51-41-05-0G, 51-40-02-0G, AND 53-00-55-2R PROCEDURE 4. (LP #0226235)

Part: DOUBLER — CORRODED (BS 1053 L29L/R) · corrosion level 2 · airframe 58,073 hrs · 41,152 cycles

CORROSION ON PRODUCTION DOUBLER ATTACHED TO FWD FACE STA 1053 BTW LONGERON 29L AND 29R AT AFT PRESSURE BULKHEAD (LOWER AREA) AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00570: CORROSION LEVEL 2. DOUBLER ATTACHED TO FWD FACE STA 1053 BTW LONGERON 29L AND 29R AT AFT PRESSURE BULKHEAD (LOWER AREA) AT AFT CARGO COMPARTMENT WAS FABRICATED PER DWG 5910130 REV ET AND REPLACED PER B717 SRM 51-41-02-0G. (LP #0225992)

Part: BULKHEAD WEB — CORRODED (BS 1053 S26L/R) · airframe 58,073 hrs · 41,152 cycles

CORROSION ON FWD LOWER FACE OF AFT PRESSURE BULKHEAD STA Y=1053 BTW L26L AND L26R AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00462: CORROSION LEVEL 1. CORROSION ON FWD LOWER FACE OF AFT PRESSURE BULKHEAD STA Y=1053 BTW L26L AND L26R AT AFT CARGO COMPARTMENT WAS REMOVED PER B717 SRM 51-10-04-0G PAR 26 C. (UT) MEASUREMENT THICKNESS WAS ACCOMPLISHED PER DC-MD/BOEING NDT SPM PART 4, 04-00-06 PAR 4 FIG 9 ON FWD LOWER FACE OF AFT PRESSURE BULKHEAD STA Y=1053 BTW L26L AND L26R AT AFT CARGO COMPARTMENT AREA WITH ORIGINAL TICKNESS IS 0.063" AND MINIMUM REMAINING THICKNESS IS 0.052" THEREFORE IS WITHIN LIMITS PER B717 SRM 53-20-08-2R PROCEDURE 2 REPAIR 2 PAR. 4.A.1 (B). (LP #0225278)

Part: WEB — CORRODED (BS 196) · corrosion level 2 · airframe 58,073 hrs · 41,152 cycles

CORROSION ON MEMBRANE STA Y=196 X=54.5 AT PAX CABIN. SUMMARY OF NRC 00618: CORROSION LEVEL 2. MEMBRANE STA Y=196 X=54.5 AT PAX CABIN WAS REPAIRED PER B717 SRM 51-70-10-2R PROCEDURE 2 REPAIR 2. (LP #0225652)

Part: FRAME — CRACKED (BS 674) · airframe 58,073 hrs · 41,152 cycles

AD. CRACK OF 0.734 IN LENGTH WAS FOUND ON THE UPPER RADIUS OF FRAME TAB ON THE OVERWING FRAME AT STA Y=674.000 RH. (IN REF CARD 5310-01436-04D, JOB #079-0004, STEP 7). SUMMARY OF NRC 00293: OVERWING FRAME AT STA Y=674.000 RH WAS REPLACED PER AMDS 5310-01436-03B. ASSOCIATED AA 5310-01436 ADDED FOR AC 9541. (LP #0221718)

Part: FLOOR SUPPORT — CORRODED (BS 164-200) · corrosion level 2 · airframe 58,073 hrs · 41,152 cycles

CORROSION ON FLOOR SUPPORT STA Y=164, Y=190, AND Y=200 X=54.5 AT PAX CABIN. SUMMARY OF NRC 00616: CORROSION LEVEL 2. FLOOR SUPPORTS STA Y=164, Y=190, AND Y=200 X=54.5 AT PAX CABIN WERE REPLACED PER B717-200 SRM 51-41-02-0G, 51-41-05-0G, AND 51-41-08-0G. (LP #0221695)

Part: FRAME — CRACKED (BS 696) · airframe 58,073 hrs · 41,152 cycles

AD. CRACK OF 0.359 IN LENGTH WAS FOUND ON THE UPPER RADIUS OF FRAME TAB ON THE OVERWING FRAME AT STA Y=696.000 RH. (IN REF CARD 5310-01436-04D, JOB #079-0004, STEP 10). SUMMARY OF NRC 00294: OVERWING FRAME AT STA Y=696.000 RH WAS REPLACED PER AMDS 5310-01436-03B. ASSOCIATED AA 5310-01436 ADDED FOR AC 9541. (LP #0221621)

Part: CUSP WEB — MECHANIC ERROR (BS 674) · airframe 58,073 hrs · 41,152 cycles

MISDRILLED ON CUSP WEB BTW STA Y=674 AT LH CABIN PAX. SUMMARY OF NRC 00426: CUSP WEB BTW STA Y=674 AT LH CABIN PAX WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #0216550)

Part: FLOOR SUPPORT — CORRODED (BS 1017-1040) · corrosion level 2 · airframe 58,073 hrs · 41,152 cycles

CORROSION ON FLOOR SUPPORT BTW STA Y=1017-1040 X=44.5 AT PAX CABIN. SUMMARY OF NRC 00604: CORROSION LEVEL 2. FLOOR SUPPORT BTW STA Y=1017-1040 X=44.5 AT PAX CABIN WAS FABRICATED PER DWG 9981474 REV.L AND REPLACED PER B717 SRM 51-41-05-0G. (LP #0216570)

Part: FLOOR SUPPORT — CORRODED (BS 1027-1054) · corrosion level 2 · airframe 58,073 hrs · 41,152 cycles

CORROSION ON FLOOR SUPPORT BTW STA Y=1027-1054 X=-54 AT PAX CABIN. SUMMARY OF NRC 00609: CORROSION LEVEL 2. FLOOR SUPPORT BTW STA Y=1027-1054 X=-54 AT PAX CABIN WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #0216555)

Part: DOOR FRAME — CORRODED (FWD CARGO) · corrosion level 2 · airframe 58,073 hrs · 41,152 cycles

CORROSION AFT PREVIOUS REPAIR DOUBLER ON FWD CARGO COMPARTMENT DOOR JAMB. SUMMARY OF NRC 00195: CORROSION LEVEL 2. NEW DOUBLER ON FWD CARGO COMPARTMENT DOOR JAMB WAS FABRICATED PER B717 SRM 53-20-15-2R PROCEDURE 6 REPAIR 6 AND REPLACED PER SRM 51-41-02-0G AND 51-41-05-0G. (LP #0212781)

Part: DOUBLER — CORRODED (CARGO DOOR FRAME) · corrosion level 2 · airframe 58,073 hrs · 41,152 cycles

CORROSION ON FWD PREVIOUS REPAIR DOUBLER ON AFT CARGO COMPARTMENT DOOR JAMB PAN. SUMMARY OF NRC 00137: CORROSION LEVEL 2. FWD PREVIOUS REPAIR DOUBLERS ON AFT CARGO COMPARTMENT DOOR JAMB PAN WERE REPLACED PER B717 SRM 53-20-15-2R PROCEDURE 7 REPAIR 7. PERFORM GVI ON REPAIR DOUBLER ON AFT CARGO COMPARTMENT DOOR JAMB PAN EVERY C CHECK PER B717 SRM 53-20-15-2R PROCEDURE 7. (LP #0209647)

Part: FRAME — CRACKED (BS 674) · airframe 58,073 hrs · 41,152 cycles

A.D. CRACK OF 0.100 IN ON UPPER RADIUS OF THE FRAME TAB ON THE OVERWING FRAME AT STA Y=674.000 LH (REF CARD 5310-01436-04B). SUMMARY OF NRC 00265: CRACK OF 0.100 IN ON UPPER RADIUS OF THE FRAME TAB ON THE OVERWING FRAME AT STA Y=674.000 LH WAS REPAIRED PER AMDS 5310-01436-02A. ASSOCIATED AA 5310-01436 ADDED FOR AC 9541. (LP #0209495)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,619 hrs · 39,918 cycles

FIRST CLASS CEILING EXIT SIGN COVER IS MISSING. MAINTAINANCE REPLACED THE COVER AS REQUIRED. AIRCRAFT IS OK FOR SERVICE. (LP #4730934)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,531 hrs · 39,836 cycles

CRACK INDICATION ON L/H VERT STAB ON HOLE 5 FROM BOTTOM -MARKED-. CONFIRMED CRACK IS IN SKIN LAYER ONLY QC5253. REMOVED LEADING EDGE VERTICAL STAB REF. B717, AMM 55-32-01. C/W ERA 609501-14AD REV ORIGINAL PERMANENT REPAIR SECTION I QC5270. REINSTALLED LEADING EDGE VERTICAL STAB REF B717 AMM 55-32-01. ASSOCIATED ERA 14-609501 ADDED FOR AC 9541. (LP #4773079)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,531 hrs · 39,836 cycles

CRACK INDICATION ON L/H VERT STAB ON HOLES 5 FROM BOTTOM -MARKED-. C/W PRI 609501-14AD REV 0 AND 1 QC 5270. C/W PRI 609501-14AD REV 2 QC 5270. FINAL ERA 609501-14AD REV ORIGINAL MATCHES ALL STEPS OF PRI 609501-14AD REV 0, 1, AND 2 QC 5270. ASSOCIATED ER/A 14-609501 ADDED FOR AC 9541. (LP #2805577)

Part: LONGERON — CORRODED (BS 904-927 L30) · corrosion level 2 · airframe 53,435 hrs · 37,127 cycles

CORROSION AT LONGERON 30 BETWEEN STA 904 AND STA 927. SUMMARY SEE NRC 088-0008:5331-2001/007 00377: REPLACED LONGERON 30 BETWEEN STA 904 AND STA 927 PER B717 SRM 51-40-02. CORROSION LEVEL:2 . (LP #2086514)

Part: NONE — NONE · corrosion level 2 · airframe 53,435 hrs · 37,127 cycles

CORROSION STA 927 TO 946 AT LONGERON 30 AND SPLICE. SUMMARY SEE NRC 088-0008:5331-2001/011 00381: REMOVED CORROSION AND CHECKED LIMITS STA 927 TO 946 LONGERON 30 PER B717 SRM 53-00-00. REPLACED SPLICED PER B717 SRM 53-20-05-2R. (LP #2085655)

Part: NONE — NONE · airframe 53,435 hrs · 37,127 cycles

THE IDG FEEDER HARNESS IS ROUTED TOO CLOSE TO THE #2 ENGINE FUEL LINE, AS INDICATED IN WORK CARD 0571-9202. THERE MUST BE A 0.39" MIN DISTANCE. SUMMARY SEE NRC 110-0001:0571-9202/010 00370: ROUTED IDG FEEDER HARNESS AS PER AMDS CARD 0571-9202. (LP #2083609)

Part: CABLE — FRAYED (L1 DOOR SLIDE) · airframe 52,812 hrs · 36,569 cycles

DURING 1L SLIDE REPLACEMENT, THE LANYARD CABLE ASSEMBLY WAS FOUND TO BE FRAYED. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE INSTALLED A SERVICEABLE LANYARD PER AMDS 2561.9004. THE AIRCRAFT IS OK FOR SERVICE. (LP #8103208)

Part: DOOR SILL — DAMAGED (AFT CARGO) · airframe 52,808 hrs · 36,565 cycles

THE AFT CARGO DOOR SILL IS DAMAGED ON THE RIGHT HAND SIDE. MAINTENANCE REPLACED THE SILL PER B717 SRM 51-40. (LP #8103207)

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,105 hrs · 32,750 cycles

RIGHT SIDE FRAME 715 SHOWS SIGNS OF A CRACK IN RADIUS WITH NDT TESTING PER 5310-01436-01C. NRC 044-0003:5310-01436-01C/001 00033: REPLACED OW FRAME AT STA 715 RT SIDE PER AMDS 5310-01436-03B. (LP #1086614)

Part: GASPER FAN — ODOR (CABIN) · airframe 45,500 hrs · 30,921 cycles

THE FLIGHT WAS DIVERTED TO RDU DUE TO A REPORTED ELECTRICAL ODOR IN THE FIRST CLASS AREA. NO SMOKE OR HAZE WAS VISIBLE AND EVEN WITH THE GALLEY POWER ISOLATED, THE ODOR WAS STILL PRESENT. THE CREW DID DECLARE AN EMERGENCY FOR THE DIVERSION. CORRECTIVE ACTION: MAINTENANCE FOUND THAT THE GASPER FAN WAS EMITTING THE ODOR THROUGHOUT THE SYSTEM AND REPLACED THE FAN (WHICH WAS ALREADY ON MEL AT THE TIME).

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 45,462 hrs · 30,896 cycles

EMERGENCY EXIT SIGN LENS LOOSE. REINSTALLED THE LENS. AIRCRAFT IS OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 45,393 hrs · 30,843 cycles

DURING A SERVICE CHECK, PERFORMED AN EMERGENCY LIGHTS TEST, FOUND SEVERAL EXIT LIGHTS THAT WOULD NOT STAY ILLLUMINATED. REPLACED THE BATTERY AND POWER SUPPLY IAW AMM 33-51. OPS TESTED GOOD IAW AMM 33-51.

Part: CHANNEL — CRACKED (LT SPOILER)

DURING AN UNSHEDULED NON ROUTINE CHECK, FOUND INBOARD SPOILER INNER CHANNEL CRACKED.

Part: POWER SUPPLY — DEFECTIVE (CABIN) · airframe 43,805 hrs · 29,791 cycles

THE AFT CABIN EMERGENCY EXIT SIGN REMAINED ON WITH THE EMERGENCY SWITCH OFF. MAINTENANCE REPLACED B5-260 EMERGENCY POWER SUPPLY PER AMM 33-51-03 AND THE SYSTEM CHECKS OK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 43,783 hrs · 29,774 cycles

DURING A SERVICE CHECK, FOUND EMERGENCY LIGHTS IN AFT EQUIP BAY WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY B5-260 IAW AMM 33-51, OPERATIONAL CHECKED GOOD. AIRCRAFT IS OK FOR SERVICE.

Part: ACCESS DOOR — CORRODED (AFT STAIR) · corrosion level 2 · airframe 43,711 hrs · 29,735 cycles

CORROSION WAS FOUND ON FWD STAIRWAY ACCESS DOOR. DAMAGED AREA WAS REPAIRED IAW ETI-17-17-136, REV 2, AND ER/A 560864-14, REV ORIG.

Part: SUPPORT FITTING — CRACKED (BS 645) · airframe 43,707 hrs · 29,733 cycles

SUPPORT FITTING ON CENTER FUEL TANK FWD FACE WAS FOUND CRACKED ON BS 645, RBL 22, AND Z-9 IN THE FWD CARGO BAY. REMOVED, DRILLED, TREATED, PAINTED, AND INSTALLED IAW SRM 51-41-05.

Part: FITTING — CRACKED (BS 661) · airframe 43,707 hrs · 29,733 cycles

CRACK ON ANGLE OF WING TO BODY FITTING, LONGERON 22L, BS 661. THE ANGLE WAS REMOVED, FABRICATED, TREATED, PAINTED, AND INSTALLED IAW ER/A 560866-14, AND ETI-17-17-134, REV 3.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 43,707 hrs · 29,733 cycles

THREE CRACK INDICATIONS WERE CONFIRMED AT ZFS 49.267, 48.267, AND 44.267. REPAIRED IAW ER/A 560869-14AD, REV ORIGINAL, AND ETI 17-17-128, REV 3.

Part: STIFFENER — CRACKED (BS 645) · airframe 43,707 hrs · 29,733 cycles

SUPPORT FITTING ON CENTER FUEL TANK FWD FACE WAS FOUND CRACKED ON BS 645, LBL 22, AND Z-9 AT FWD CARGO BAY. THE STIFFENER WAS REMOVED, FABRICATED, DRILLED, AND INSTALLED IAW SRM 51-41-05. NO FOUND LEAKS WERE FOUND.

Part: SKIN — CRACKED (BS 1022) · airframe 43,707 hrs · 29,733 cycles

CRACKED EXTERNAL FUSELAGE SKIN BS 1022 AND LONGERON 14L. REPAIRED IAW ETI-17-17-118, REV 2, AND ER/A 559574-14, REV ORIGINAL, ER/A 559574-14, REV ORIGINAL.

Part: DOUBLER — DAMAGED (VERTICAL STAB) · airframe 43,707 hrs · 29,733 cycles

DISTRESS LT HOLES (7 EA) ON REPAIR DOUBLER LE STA ZFS=52.267 VERTICAL STABILIZER. REPAIR DOUBLER ON LE STA ZFS=52.267 VERTICAL STABILIZER WAS REPLACED PER SRM 55-30-01 2R REP 7 AND SERVICE GENERAL REPAIR DRAWING SG95550001 REV B.

Part: SKIN — CRACKED (BS 1076) · airframe 43,707 hrs · 29,733 cycles

CRACKED FUSELAGE SKIN BS 1076, LONGERON 14R. THE SKIN WAS REPAIRED IAW ETI-17-17-113 REV 1, AND ER/A 559566-14 REV ORIGINAL.

Part: RIB — CRACKED (WING) · airframe 43,707 hrs · 29,733 cycles

DURING SLAT DOOR MECHANISM REMOVAL PER CARD 00229 CRACKED RIB WAS FOUND. RIB WAS REPLACED PER SRM 51-40-05, 51-41-02, 51-41-05, SOPM 20-10-7, AND IPC 57-41-57-01 FIG 101.

Part: SKIN — CRACKED (RT WING) · airframe 43,707 hrs · 29,733 cycles

CRACK ON LWR SKIN FROM STA XRS=170 TO XRS=137 AT TRAILING EGDE RT WING (AD). CRACK ON LWR SKIN FROM STA XRS=170 TO XRS=137 AT TRAILING EGDE RT WING WAS REPLACED PER SRM 51-41-01, 51-41-02, 51-41-05, AND DWG 5912144 REV AN.

Part: INTERCOSTAL — CRACKED (CARGO DOOR) · airframe 43,707 hrs · 29,733 cycles

CRACKED INTERCOSTAL BS 427 BTW BEAM 1 AND 2 IN THE FWD CARGO DOOR. THE INTERCOSTAL WAS REPLACED IAW SRM 51-41-02, AND DWG 9957664, REV N.

Part: FRAME — CRACKED (BS 675) · airframe 43,707 hrs · 29,733 cycles

CRACKED REPAIR DOUBLER ON FRAME FORMER STA 675 BTW AND LONGERON 26R AT CENTER FUSELAGE AREA.REPAIRED IAW SRM 51-70-11-2R.

Part: FLOOR PANEL — BROKEN · airframe 43,707 hrs · 29,733 cycles

BROKEN FLOOR PANEL 223KF. THE FLOOR PANEL WAS REPLACED IAW SRM 53-20-50-2R, REP 3.

Part: FRAME — CRACKED (BS 1037) · airframe 43,707 hrs · 29,733 cycles

CRACKED FRAME BS 1037 BETWEEN LONGERONS 16R TO 18R. A REPAIR WAS ACCOMPLISHED IAW SRM 53-20-07-2R-4.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 43,707 hrs · 29,733 cycles

CORROSION ON COUNTERSINK ON FUEL ACCESS PANEL : BUSHINGS FABRICATED IAW SRM 57-10-01-2R-2, CONDITION II AND INSTALLED IAW SRM 57-10-01-2R PROCEDURE 2 STEP 5 (B) 3.

Part: FERRULE — DAMAGED (CABIN) · airframe 43,707 hrs · 29,733 cycles

DELAMINATION ON FLOOR PANEL IN THE CABIN. FERRULE REPLACED IAW SRM 53-20-50-2R, REP 3.

Part: FLOOR PANEL — DELAMINATED (COCKPIT) · airframe 43,707 hrs · 29,733 cycles

DELAMINATION ON FLOOR PANEL 211ALF AT COCKPIT. THE FLOOR PANEL WAS REPLACED IAW SRM 53-20-50-2R, REP 3.

Part: LONGERON — CRACKED (BS 1022) · airframe 43,707 hrs · 29,733 cycles

CRACKED LONGERON 17L, BS 1022. A NEW LONGERON, AND REPAIR SPLICE WERE INSTALLED IAW SRM 53-00-05-2R-2, AND 51-41-05.

Part: DOOR FRAME — CRACKED (NLG) · airframe 43,707 hrs · 29,733 cycles

CRACKED DOOR FRAME ON FWD SECTION RT & LT SIDES FRAME 47 AT THE NLG WHEEL WELL AREA. THE DOOR FRAME WAS REPAIRED IAW SRM 53-10-14, FIG 201-R2. HFEC INSPECTION WAS ACCOMPLISHED IAW NDT SPM 06-10-06-10-01. NO CRACKS WERE FOUND AROUND CUT OUT.

Part: CUSP WEB — DAMAGED (BS 617-655) · airframe 43,707 hrs · 29,733 cycles

ELONGATED LIGHTENING HOLES ON THE CUSP WEB BS 617 - 636 AND BS 636 - 655. THE CUSP WEB WAS REPAIRED.

Part: CUSP WEB — CORRODED (BS 470) · airframe 43,707 hrs · 29,733 cycles

CORROSION ON THE CUSP WEB BS 470 BETWEEN RBL 56 TO 60. THE CUSP WEB WAS REPAIRED IAW SRM.

Part: BEAM — CRACKED (L1 DOOR) · airframe 43,707 hrs · 29,733 cycles

CRACK ON BEAM NR 7, AFT EDGE AT THE L1 DOOR. THE BEAM WAS REPAIRED IAW SRM 52-10-02-2R-13, FIG 201, SHEET 3.

Part: PAN — CRACKED (CARGO DOOR FRAME) · airframe 43,707 hrs · 29,733 cycles

CRACKED OUTER PAN (FWD EDGE) BS 370 BETWEENS BEAM 1 AND 2 AT FWD CARGO COMPARTMENT DOOR. THE PAN WAS REPAIRED IAW SRM. 52-30-02-2R PROCEDURE 3.

Part: BEAM — CRACKED (NR 1) · airframe 43,707 hrs · 29,733 cycles

CRACK ON BEAM NR 1 , AFT EDGE AT PASSENGER ENTRANCE. THE BEAM WAS REPAIRED IAW SRM 52-10-02-2R, REPAIR 7, FIG 201.

Part: FLOOR SUPPORT — CRACKED · airframe 43,707 hrs · 29,733 cycles

CRACK ON HAT CHANNEL OF FLOOR PANEL 222 ALF. REPAIRED IAW SRM 53-20-50-2R, REPAIR 5.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,683 hrs · 25,867 cycles

EMERGENCY LIGHTS AT BS 870 - 889 ARE INOPERATIVE. REPLACED THE BATTERY PACK B5-231.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,874 hrs · 24,409 cycles

LT & RT FWD OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY IN POWER SUPPLY IAW AMM 33-51. CHECKS NORMALLY.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,210 hrs · 23,829 cycles

DURING LINE CHECK, NOTED THE FORWARD CABIN EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND BATTERY IAW AMM 33-51 AND OPS CHECKED NORMAL.

Part: LIGHT — BROKEN (CABIN) · airframe 34,766 hrs · 22,594 cycles

R2 DOOR EMERGENCY EXIT LIGHT BROKEN. R & R LIGHT IAW AMM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 34,181 hrs · 22,221 cycles

LOWER FS EXTERIOR CANTED KEEL LT SIDE AT FS 695 CRACKED UPPER ANGLE. REPAIRED ANGLE IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 34,181 hrs · 22,221 cycles

LOWER FUSELAGE EXTERIOR CANTED KEEL LT SIDE FS 660 INTERNAL CRACKED UPPER ANGLE. REPAIRED ANGLE IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 34,181 hrs · 22,221 cycles

CUSP WEB CRACKED AT STATION 218, RBL 44. REPAIRED WEB IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 34,181 hrs · 22,221 cycles

LOWER FS CANTED KEEL RT SIDE FS 660 CRACKED UPPER ANGLE. REPAIRED ANGLE IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,181 hrs · 22,221 cycles

LT SEAT TRACK CORRODED BETWEEN STATION 823 TO STATION 899. R & R SEAT TRACK IAW AMM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 34,181 hrs · 22,221 cycles

LOWER FS CANTED KEEL RT SIDE FS 678 INTERNAL CRACKED UPPER ANGLE. REPAIRED ANGLE IAW SRM.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 34,181 hrs · 22,221 cycles

R1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. SECURED CONNECTOR IAW MM.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 34,181 hrs · 22,221 cycles

EMERGENCY EXIT SIGNS ABOVE OVERWING DOOR INOPERATIVE. SECURED CONNECTOR IAW AMM.

Part: RETAINER — CRACKED (COCKPIT) · airframe 34,181 hrs · 22,221 cycles

CAPTAIN`S EMERGENCY ESCAPE LINE INNER RETAINER CRACKED. REPAIRED RETAINER IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 34,181 hrs · 22,221 cycles

AFT FS FRAME SUPPORT ANGLE CRACKED AT BS 1022 BETWEEN LONGERON 16L. R & R ANGLE IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 34,181 hrs · 22,221 cycles

CUSP WEB CRACKED BETWEEN BS 665 TO BS 675 LBL 44. REPAIRED WEB IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 34,181 hrs · 22,221 cycles

MAIN FS FRAME SUPPORT ANGLE CRACKED AT BS 1022 LONGERON 16R. R & R ANGLE IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 34,181 hrs · 22,221 cycles

RT KEEL UPPER ANGLE CRACKED AT FS 695. REPAIRED ANGLE IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 34,181 hrs · 22,221 cycles

FLOOR WEB CRACKED BETWEEN BS 813L & 832L. REPAIRED WEB IAW SRM.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 34,181 hrs · 22,221 cycles

LT SIDE WALL SUPPORT BRACKET CRACKED AT BS 200 LONGERON 15L. REPAIRED BRACKET IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 34,181 hrs · 22,221 cycles

FUSELAGE FRAME SUPPORT ANGLE CRACKED AT BS 1022, LONGERON 16 UPPER. R & R ANGLE IAW SRM.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 34,181 hrs · 22,221 cycles

LONGERON CORRODED AT STATION 927, LONGERON 30. R&R LONGERON IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 34,181 hrs · 22,221 cycles

AFT CARGO COMPARTMENT FWD BULKHEAD PANEL SUPPORT LT INTERCOSTAL CRACKED. R&R INTERCOSTAL IAW SRM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 34,181 hrs · 22,221 cycles

R1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING FASTENER CORRODED. R&R FITTING IAW SRM.

Part: SUPPORT BRACKET — BROKEN (FUSELAGE) · airframe 34,181 hrs · 22,221 cycles

WING TO BODY FAIRING RIB SUPPORT BRACKET BROKEN AT STATION 636, LONGERON 19R. R&R BRACKET IAW SRM.

Part: SUPPORT BRACKET — BROKEN (FUSELAGE) · airframe 34,181 hrs · 22,221 cycles

WING TO BODY FAIRING RIB SUPPORT BRACKET BROKEN AT STATION 636, LONGERON 19L. R&R BRACKET IAW SRM.

Part: ANGLE — CRACKED (RT MLG WW) · airframe 34,181 hrs · 22,221 cycles

RT MLG WW CUTOUT FWD LOWER AREA ANGLE CRACKED. R&R ANGLE IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 34,181 hrs · 22,221 cycles

RT WW CUTOUT AFT VERTICAL WEB CRACKED. REPAIRED WEB IAW SRM.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 34,181 hrs · 22,221 cycles

AFT FS INTERNAL, LT VENT BOX, UPPER AFT SUPPORT BRACKET CRACKED. R&R BRACKET IAW SRM & DRAWING.

Part: FRAME — CORRODED (FUSELAGE) · airframe 34,181 hrs · 22,221 cycles

FRAME CORRODED AT STATION 908, LONGERON 30. REPAIRED FRAME IAW SRM.

Part: SIGN — MISSING (CABIN) · airframe 32,722 hrs · 21,310 cycles

R1 DOOR EMERGENCY EXIT SIGN MISSING. INSTALLED COVER PER MM.

Part: PIN — LOOSE (L1 DOOR) · airframe 32,239 hrs · 20,992 cycles

L1 DOOR EMERGENCY EVAC SLIDE PIN LOOSE. SECURED PIN PER AMM.

Part: PIN — LOOSE (L1 DOOR) · airframe 32,322 hrs · 21,047 cycles

L1 DOOR EMERGENCY EVAC SLIDE PIN LOOSE WHEN GIRT BAR REMOVED FROM FLOOR FITTINGS. RE-SECURED PIN PER AMM.

Part: PIN — LOOSE (GALLEY) · airframe 32,158 hrs · 20,938 cycles

STRONG HOT ELECTRIC ODOR WHEN COFFEE POTS SET TO BREW. ODOR STOPPED WHEN F/A REMOVED POWER FROM COFFEE POTS. SECURED GROUND PIN IN WIRING HARNESS FOR COFFEEMAKER PER SWPM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 31,330 hrs · 20,400 cycles

FWD BOTTOM EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT IAW MM.

Part: COVER — LOOSE (EVAC SLIDE) · airframe 3,080 hrs · 20,108 cycles

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

Part: COVER — BROKEN (EVAC SLIDE) · airframe 30,834 hrs · 20,078 cycles

R1 DOOR EMERGENCY EVAC SLIDE COVER BROKEN. REPAIRED COVER PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN)

COCKPIT EMERGENCY LIGHT DOES NOT ILLUMINATE WITH PRE-FLIGHT CHECK. REMOVED AND REPLACED B5-123 BATTERY PACK ASSEMBLY, OPS CHECK GOOD REF MM 33-50.

Part: PAN — CORRODED (FUSELAGE)

FORWARD CARGO DOOR JAMB LOWER PAN, CORROSION. ACCOMPLISHED DOOR JAMB LOWER PAN REPLACEMENT PER B717 SRM 53-00-00 AND 53-20-15.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE)

AFT CARGO COMPARTMENT FORWARD FACE SUPPORT ANGLES, STA 908, LONG 29L TO 29R, CORROSION. ACCOMPLISHED FORWARD FACE SUPPORT ANGLES SPLICE REPAIR PER B717 SRM 51-10-04 AND 53-00-06.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CENTER RIGHT FLOOR SUPPORT, STA 148 TO 200, RBL 7, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-40-02.

Part: FITTING — CORRODED (CABIN)

R1 DOOR FORWARD AND AFT GIRT BAR FITTINGS, CORROSION. ACCOMPLISHED FORWARD AND AFT GIRT BAR FITTINGS REPLACEMENT PER B717 SRM 53-00-00 AND 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 160 TO 200, RBL 53, CORROSION. ACCOMPLISHED CABIN FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02 AND 51-41-05.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 148 TO 200, LBL 7, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-01.

Part: WEB — CORRODED (FUSELAGE)

SUB FLOORING WEB, STA 156 TO 200, BL 0, CORROSION. ACCOMPLISHED WEB DOUBLER REPAIR PER B717 SRM 51-10-04, 53-00-00 AND 51-70-10.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CENTER FLOOR SUPPORT, STA 200, BL 0, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-10-04, 53-00-00, 51-41-02 AND 54-41-05.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FLOOR SUPPORT, STA 180, RBL 10 TO 40, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02 AND 51-41-05.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 200, RBL 10 TO 44, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT, STA 160 TO 200, RBL 44, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 53-00-00 AND 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FLOOR SUPPORT ANGLE, STA 237, BL 0, CORROSION. ACCOMPLISHED FLOOR SUPPORT ANGLE REPLACEMENT PER B717 53-00-00, 51-10-04, 51-22-01 AND 51-41-05.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FLOOR SUPPORT, STA 200 TO 256, LBL 15, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02 AND 51-41-05.

Part: LENS — MISSING (CABIN)

EMERGENCY LIGHT LENS MISSING 1 AND 2 D. RELAMPED AND REPLACED LENS OPS CHECK GOOD REF AMM 33-51.

Part: SIGN — MISSING (CABIN)

EXIT SIGN MISSING ON LT SIDE O/W EXIT ON ROW 22. (TEMP SIGN INSTALLED PER EA 17-33-03268IR REPLACE WITH PROPER SIGN AFTER 1 FLT CYCLE). INSTALLED LENS REF 33-28.

Part: LANYARD — MISINSTALLED (EVAC SLIDE)

R1 DOOR GIRT BAR FABRIC PULLED BACK SO BAR IS OVERLY EXPOSED CABLE LINER IS INSTALLED IMPROPERLY. REINSTALLED GIRT BAR LANYARD CORRECTLY - REF AMM 25-61. OK FOR SERVICE.

Part: WIRE — CUT (CABIN)

ROW 31 SEAT EMERGENCY LIGHTS DID NOT ILLUMINATE. FOUND WIRE CUT, SPLICE WIRE PER B717 SWPM 20-10-03, OPS CHECK GOOD.

Part: BATTERY — DISCHARGED (CABIN)

DURING SVC CHECK FOUND EMERGENCY LIGHTS FOR RT BUSINESS CLASS AND BACK TO ROW 15 INOP. T/S FOUND BATTERY SUPPLY AT STA 341 V1-118 INOP. REMOVED AND REPLACED BATTERY SUPPLY & BATTERY ASSY IAW 33-51-03. OP'S NORMAL PER 33-51-00-710-801.

Part: LIGHT — MISSING (CABIN)

LENS AND BULBS FOR ESCAPE PATH LIGHT ON SIDE OF 1D IS MISSING. REPLACED LENS (RED) AND BULBS, OPS CHECK GOOD REF AMM 33-51.

Part: STRAP — CRACKED (FUSELAGE)

AFT FUSELAGE COMPARTMENT CANTE FRAME SUPPORT STRAP AT STA 1178, BETWEEN LONG 16 AND 17 RIGHT HAND CRACKED. INSTALLED FORMED ANGLE REPAIR AT FUS 1178 BETWEEN LONG 16 AND 17 RIGHT HAND PER SRM 51-70-11 FIG 201.

Part: STRAP — CRACKED (FUSELAGE)

AFT FUSELAGE COMPARTMENT CANTE FRAME SUPPORT STRAP AT STA 1178, BETWEEN LONG 16 AND 17 LEFT HAND CRACKED. INSTALLED FORMED ANGLE REPAIR AT FUS 1178 BETWEEN LONG 16 AND 17 LEFT HAND PER SRM 51-70-11 FIG 201.

Part: EEC — MALFUNCTIONED (RT ENGINE)

EPR FLUCTUATIONS OF +/- .08 AND TGT FOLLOWED INDICATIONS OF +/- 40 DEG. REMOVED AND REPLACED RIGHT ENGINE EEC, NO DEFECTS NOTED REF 73-21.

Part: SLIDE — MALFUNCTIONED (R-1 DOOR)

SLIDE DID NOT FULLY DEPLOY ON TEST. REMOVED AND REPLACED SLIDE ASSY.

Part: DISPLAY — FAILED (NR 4)

NR 4 DU FAILED IN FLIGHT WITH SMOKE IN COCKPIT ONLY. REMOVED AND REPLACED NR 4 DU. DISPLAY TESTS PASSED. ALSO CLEANED REMAINING DU COOLING INLETS. INSPECTED INST COOLING FAN & FILTER, NO DEFECTS FOUND. OK FOR SERVICE. REF 31-43, 31-61. P/N OFF/ON 4082170-912, S/N OFF 02770892, S/N ON 31491628.

Part: LINE — CRACKED (HYD SYSTEM)

LOSS OF HYD PRESSURE AND QUANTITY AFTER TAKE OFF. FOUND CRACKED END ON GROUND SRV RETURN/PRESS LINE. REPAIRED END OF TUBING WITH PERM-A-SWAGE FITTING REF M/M 20-10 SERVICED HYD LEAK AND OPS CK GOOD. RAN NR 2 ENG, OPS CK EDP, OPS CK GOOD.

Part: SHUTOFF VALVE — INOPERATIVE (RT ANTI ICE SYS)

PILOT GOT A RIGHT ANTI-ICE DISAGREE LIGHT ON THE EAD. REMOVED AND REPLACED THE RIGHT ENGINE ANTI-ICE VALVE.

Part: SKIN — DENTED (BS 235)

DENT IN FUSELAGE AT STA 235.5, 4 INCH ABOVE LONG 18L. 3 INCH DIA BY .1 DEEP DENT HAS CREASED AT FRAME 237. INSTALLED REPAIR AT BS 237 TO 252 AND LONG 17 AND 18. IAW SRM 53-00-01 SIZE OF REPAIR 15.2500 INCH X 14.1250 INCH.

Part: ENGINE — FIRE (NR 2)

TAIL PIPE FIRE WHILE ATTEMPTING TO START NR 2 ENGINE. PERFORMED STEP'S OT LINED IN ROLLS ROYCE TECHNICAL VARIANCE 5974. INSPECTED AND CLEANED ENGINE IAW MM CHP 71-00-2 AND STARTED ENGINE WITH SUCCESSFUL TIMES, NO FAULTS NOTED ON EEC NR 2 ENGINE FOR SERVICE AT THIS TIME.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY LIGHTS OUT IN FORWARD CABIN, AT L-1 DOOR AND R1 DOOR. REMOVED AND REPLACED 35-118 BATTERY PACK OPS CHECK GOOD.