N947AT
Registered owner: DELTA AIR LINES INC, GA (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
ATB- RETURNED TO DTW DUE TO A LEFT HYDRAULIC QUANTITY LOW MESSAGE. MAINTENANCE FOUND THE LEFT SYSTEM ACCUMULATOR LEAKING AND REPLACED SAME. ALL OPERATIONAL AND LEAK CHECKS NORMAL. (8424352) (AIRCRAFT GROUNDED).
EMERGENCY EXIT SIGN ON CEILING BETWEEN 1B AND 1C IS DAMAGED. REPLACED DAMAGED EXIT SIGN IAW AMM 33-51. (8182268)
GIRT BAR BRACKETS HARD TO OPERATE / LOCATIONS:601. CLEANED AND LUBED DOOR 1L GIRT BAR LATCH CHECKS GOOD REF B717 MM 25-61 OK FOR SVC (1306981).
CRACK ON EXTERNAL SKIN, BS 1087, BTW L-13R AND L-14R AT AFT FUSELAGE. PERMANENT REPAIR AND PRI 630164-14 REV. 3. (1291355)
SHIP 9507 FUSELAGE / SKIN / STA Y=1087, L=13R & L=14R / CRACK. CORRECTIVE ACTION: ACCOMPLISH ER/A 630164-14 (1290083)
IN REF. TO AMDS 5211-4001: EMERGENCY SLIDE PACK WAS FOUND UNFOLDED, DOOR L1 WAS REPLACED UNDER AMDS 97-2561-9-0003 AND AMDS 2561- 9004 (1281137)
INSPECTION: PUNCTURE ON FWD MOVABLE VANE LOWER SURFACE AT LT WING. FWD MOVABLE VANE LOWER SURFACE AT LH WING WAS REPAIRED IAW SRM 57-53-01 (1277612).
CRACK SKIN INSIDE OF ACCESS PANEL 370BL FWD /UPPER CORNER AT VERTICAL STABILIZER DORSAL FIN. CORRECTIVE ACTION: UPPER CORNER AT VERTICAL STABILIZER DORSAL FIN WAS REPAIRED PER B717 SRM 55-30-01 (1278507)
BROKEN WIRES ON ESCAPE SLIDE LANYARD ASSEMBLY (2 EA) AT R1 & L1 DOOR. LANYARDS ASSEMBLIES AT L1 DOOR AND R1 DOOR WERE REPLACED & VERIFIED IAW AIPC 25-61-01-01 TEM 95 & AIPC 25-61-03 (1275291).
RETURNED TO ATLANTA DUE TO A LEFT GEAR UNSAFE INDICATION. PERFORMED TROUBLE SHOOT PER B717 FIM 32-60. REPLACED EMERGENCY RELEASE ROLLER FOR LEFT GEAR. TEST GOOD.(7707462)
RETURNED TO AGS DUE TO A LEFT GEAR UNSAFE INDICATION. MAINTENANCE REPLACED THE LEFT DOOR UP AND LATCHED SENSOR. CYCLED GEAR OPS CHECK NORMAL.(7707452)
AFT OVERWING (L&R) EXIT LIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACKS B5-119 & B5-230. OPERATIONAL CHECK IS NOW NORMAL REF B717 AMM 33-51. (LP #6520466)
-AD- DUE TO CRACK INDICATION FOUND DURING INSP, COMPLIED WITH AMDS CARD 5720-01103-01B. REQUIRES COMPLETION OF PRI 624259-14. COMPLIED WITH PRI 624259-14AD REV 0, 1, & 2. COMPARED PRI 324259-14AD REV 0, 1, & 2 WITH ERA 624259-14AD REV ORIG AND ALL ITEMS MATCH. ALL RII ITEMS CW. REF LOG PAGE 0911925 FOR MONITOR. ASSOCIATED ER/A 14-624259 ADDED FOR AC 9507. (LP #6520422)
-AD- CRACK WAS FOUND IN LOWER SPAR CAP NEAR XRS=164 DURING INSP OF LT WING REAR SPAR INSP AMDS 5720-01103-01A. "CONTACT LIAISON ENGINEERING FOR REPAIR PRIOR TO FURTHER FLIGHT" FC 5720-01103. COMPLIED WITH PRI 624256-14AD REVS 0, 1, 2, 3, 4, & 5. COMPARED PRI 624256-14AD REVS 0, 1, 2, 3, 4, & 5 WITH ERA 624256-14AD REV ORIG. ALL ITEMS MATCH. COMPLIED WITH ERA 624256-14AD REV ORIG. ALL RII ITEMS CW. REF LOG PAGE 0911920 FOR MONITOR. ASSOCIATED ER/A 14-624256 ADDED FOR AC 9507. (LP #6520421)
-AD- COMPLY WITH ERA 623716-14AD REV ORIGINAL. SUMMARY NRC 002-0001:0514-2001/008 00009: COMPLIED WITH ER/A 623716-14AD REV 0, PRI REV 0, 1, AND 2. ENSURED PRI AND FINAL ERA MATCH. (LP #0794140)
WHILE PERFORMING W/C 2740-01114-07, THE JACKSCREW DID NOT STOP AUTOMATICALLY AND CONTACTED THE UPPER STOP. HORIZ STAB ADJ REQUIRED PER B717 AMM 27-40-00 820-801 & INSPECTION OF THE JACK SCREW REQUIRED PER B717 AMM 27-41-04 220-802. C/W INSPECTION OF JACKSCREW PER B717 AMM 2741-04-220-802. ADJUSTED HORIZ STAB PER B717 AMM 27-40-00 820-801. ALL RII ITEMS COMPLETE QC 5306. (LP #6918044)
F/O BRIEFCASE LIGHT IS SPARKING INTERNALLY. MAINTENANCE REPLACED THE F/O BRIEFCASE LIGHT IAW B717 AMM 33-16. OPERATIONAL CHECK WAS GOOD. AIRCRAFT IS OK FOR SERVICE. (LP #6723386)
WHILE WORKING A.A. WORKCARD 2740-01114-07 HORIZONTAL JACK SCREW INSPECTION FAILED ONLY DURING ALTERNATE NOSE UP. HITS THE UPPER STOP. WITH PRIMARY SWITCH WORKS OK REF B717 AMM 27-40-00-820-801. ADJUSTED HORIZONTAL STABILIZER TRIM SYS & SHUT OFF CONTROLS PER B717 AMM 27-40-00-820-801. HORIZONTAL STAB TRIM SYST & S/O CONTROLS RIG CHECK ACCOMPLISHED. INSTALLED SAFETY CLIPS AT TURNBUCKLES (E) & (H) PER B717 AMM 27-40. COMPLETE STEPS G (7)(C) ALTERNATE LIMIT SWITCH (AG) ADJ. REF B717 AMM 27-40-00. COMPLETE STEPS G (7-21) OF ALTERNATE LIMIT SWITCH ADJ OF B717 AMM 27-40-00. COMPLETED STEPS G (22-24) NOSE UP STOP BOLT AND ADJUSTED ALT LIMIT SWITCH RE B717 AMM 27-40-00. PERFORMED RII FOR B717 AMM 27-40-00 STEPS G (22-24) NOSE UP STOP BOLT AND ALT LIMIT SW ADJUSTMENTS (QC1511). REPLACED STAB ALTERNATE UP SWITCH PER B717 AMM 27-40(478876). C/W B717 AMM 27-40-00-820-801 FROM STEP G.25 THRU G.38. ALL RII'S FOR THIS TASK C/W (QC4028). ASSOCIATED AA 2740-01114 ADDED FOR AC 9507. (LP #0307321)
REF LOG #0286119: C/W ER/A 617263-14 REV ORIG. C/W ER/A 617263-14 REV ORIG SECTION II STEPS 1 AND 2. NO FURTHER DEFECTS NOTED. CUT OUT DAMAGED SKIN AND DRILLED REPAIR DOUBLER PER ER/A 617263-14 REV ORIG SECTION II STEP 3. C/W DVI OF DENTS REF STEP 4 SECTION II. NO DISCREPENCIES NOTED. STEP 4 HFEC C/W ON LOG 5414770. FABRICATED, PAINTED, AND INSTALLED REPAIR PARTS PER ER/A 617263-14 REV ORIG AND B717 SRM 53-03-01-2R-1 FIG 208. RESTORED FINISH PER B717 SRM 53-03-01-2R-1. C/W ER/A 617263-14 REV ORIG SECTION II PERMANENT REPAIR USED B717 SRM 53 -03-01-2R-1 FIG 208 CLASS II PERMANENT REPAIR. LEFC INSP REQUIRED: INITIAL 28,000 FC AND REPETITIVE 15,000 FC. ASSOCIATED ER/A 14-617263 ADDED FOR AC 9507. (LP #0297248)
RT MAIN GEAR WHEEL WELL DOOR JAMB FWD CHANNEL WAS FOUND CRACKED / DAMAGED. MAINTENANCE CLEANED UP DAMAGE AND INSPECTED PER B717 SRM 53-20-02-2R PROC 3. CRACK IN UPPER CHANNEL AREA MEASURED APPROX. 0.25IN. STOP DRILLED CRACK PER B717 SRM 53-20-02-2R REPAIR 3. C/W HFEC OF CUTOUT PER B717 SRM 53-20, NO CRACKS FOUND. REMOVED RIGHT MAIN GEAR, FWD DOOR FRAME, DRILLED UP, AND INSTALLED RIGHT MAIN GEAR FWD DOOR FRAME PER BOEING DRAWING 5910784U6. CHECKED ADJUSTMENT OF RT DOOR OPEN PROX SENSOR IAW B717 AMM 32-61. GAP & INDUCTANCE CHECK OK. ADJUSTED RT MLG DOOR LATCH PER B717 AMM 32-34. JACKED AIRCRAFT AND SWUNG GEAR SEVERAL TIMES. ALL INDICATIONS NORMAL. (LP #5444407)
LIGHTS OF WALKWAY PATH DO NOT TURN ON AT AFT ACCESORIES COMPARTMENT. SUMMARY OF NRC 00214: CONNECTOR R5-1211 WAS CONNECTED CORRECTLY PER B717 WDM 33-51-14. THEN OPERATIONAL TEST WAS PERFORMED PER B717 AMM 33-51-00 710-801. SATISFACTORY TEST. LIGHTS OF WALKWAY PATH AT AFT ACCESORY COMPARTMENT TURN ON. (LP #2961686)
OUT SERVICE CEILING EMERGENCY LIGHT AT ROWS 29, 26, 22, 20, 19, 15, AND 12. ALSO OUT SERVICE LOWER EMERGENCY SIGN OF AFT RH OVERWING EXIT DOOR. SUMMARY OF NRC 00208: OPERATIONAL TEST OF THE EMERGENCY LIGHTING SYSTEM B717 AMM 33-51-00 710-801 FIGURE 501 (SHEET 2 OF 2). THE SEQUENCE OF LIGHTS TURN ON CORRECTLY. AND LOWER EMERGENCY SIGN OF AFT RH OVERWING DOOR WAS CONNECTED CORRECTLY PER B717 AMM 33-51-05 400-801. STEP 1. (B). TEST OK. (LP #2960290)
ER/A 611604-14; WINGS / OUTER WING / L.E. RHS / SKIN XOS 250-260 / DENT. ER/A 611604-14 HAS BEEN REVISED CURRENT STATUS IS REV. A. (2960169)
DURING PC POWER SYSTEM OPERATIONAL TEST AT EMERGENCY EXITS; SEAT RH AND LH WAS FOUND TURNED OFF. STATUS LEDS (GREEN LIGHT) OF MOUNTED OUTLED UNID (OU) AT PASSENGER SEAT ROW 20 LH. SUMMARY OF NRC 00195: MOUNTED OUTLED UNID (OU) AT PASSENGER SEAT ROW 20 LH WAS INSTALLED CORRECTLY PER B717-200 AMM 24-55-03. TEST OK. ASSOCIATED AA 5310-01436 ADDED FOR AC 9507. (LP #2957009)
CORROSION WAS FOUND ON FRAME STA Y=1022 BTW LONG 29LH-29RH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 0183: CORROSION LEVEL 2. FRAME STA Y=1022 BTW LONG 29LH-29RH AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 3 REPAIR 3. PERFORM AN INITIAL VISUAL INSPECTION 25,000 CYCLES AFTER THIS REPAIR IS COMPLETED, AND A REPETITIVE INSPECTION EVERY 6,500 CYCLES PER B717-200 SRM 53-20-07-2R PROCEDURE 3, REPAIR 3 STEP 6. (LP #2955353)
CORROSION ON FRAME STA Y=889 LONG 29LH-29RH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 0185: CORROSION LEVEL 2. FRAME STA Y=889 LONG 29LH-29RH AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 3. (LP #2955290)
CORROSION ON FRAME STA Y=889 LONG 29LH-29RH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 0185: CORROSION LEVEL 2. FRAME STA Y=889 LONG 29LH-29RH AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 3. THE REPAIR'S SPECIFIED MAINTENANCE REQUIREMENTS ARE A VISUAL INSPECTION INITIALLY WITHIN 25,000 CYCLES AFTER INSTALLATION WITH REPETITIVE INTERVAL OF 6,500 CYCLES AS PER B717 SRM 53-20- 07-2R-3, PAR 6. A. (LP #2955487)
CORROSION ON FRAME CLIP AT STA Y=1022 BTW LONG 30 AND LONG 29L. AREA EXCEEDS MORE THAN 50 PERCENT OF THE ALLOWED DAMAGE PER B717-200 SRM 53-00-00-1A PAR 4. SUMMARY OF NRC 00180: CORROSION LEVEL 2. FRAME CLIP AT STA Y=1022 BTW LONG 30 AND LONG 29L AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-00-06-2R PROCEDURE 2 AND 53-20-06-2R PROCEDURE 2. (LP #2954413)
TORN KEVLAR CABLE OF SLIDE RELEASE MECHANISM INSIDE TAILCONE. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY OF NRC 00138: KEVLAR CABLE OF RELEASE MECHANISM INSIDE TAILCONE WAS REPLACED PER B717-200 AMM 53-52-01. (LP #2950442)
CORROSION ON GUSSET OF DOOR JAMB PAN BTW STA Y=994 AND LONG 29R AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00122: CORROSION LEVEL 2. GUSSET OF DOOR JAMB PAN BTW STA Y=994 AND LONG 29R AT AFT CARGO COMPARTMENT WAS REPLACED PER DWG 5913537 REV D AND B717 SRM 51-41-05-0G, 51-41-07-0G, AND 51-41-08-0G. (LP #2948498)
UPPER EMERGENCY LIGHTS OVER WING EXITS ARE INOPERATIVE. MAINTENANCE RPLACED THE EMERGENCY LIGHT BATTERY PACK STA 726 PER B717 33-51. OPERATIONAL CHECK WAS GOOD. (LP #4703548)
ON WALK-AROUND FOUND AFT CARGO DOOR FRAME DAMAGE JAMB AREA. INSPECTED DAMAGE AREA. BLENDED IAW SRM 52-30-02-R PROCEDURE 8. PERFORMED TEMP REPAIR IAW ERA 609141-14 SECTION I. ENGR APPROVED PER DAL PS 500-5-1-NO 04. ASSOCIATED ER/A 14-609141 ADDED FOR AC 9507. COMPLETED STEP 1 TO STEP 6 PER ERA 609141-14 SECTION III. C/W HFEC AND BHEC IAW ERA 609141-14 REV 0 SECTION III STEPS 7 AND 8. ONE HOLE HAS CRACK INDICATION, 3RD HOLE BELOW SPLICE (MARKED). COMPLETED STEPS 9 AND 10 PER ER/A 609141-14 SECTION III REV 0. COMPLETED STEP 11 PER ERA 609141-14 SECT. III. COMPLETED STEP 12 PER ERA 609141-14 SECTION III. COMPLETED STEP 13 PER ERA 609141-14 SECTION III. COMPLETED STEPS 14-20 PER ERA 609141-14 SECTION III. C/W WITH ERA 609141-14 REV 0. QC 1436 O.K. TO CLOSE MONITOR. (LP #4666545)
CABIN STANDBY EMERGENCY LIGHTING IS MISSING TWO LENS COVERS (LOC ROW 22 AND 26). FORWARD MISSING CABIN STANDBY EMERGENCY LIGHTING TO MEL 33-52-01. PLACARDS INSTALLED. (LP #4154618)
THE OVERHEAD EMERGENCY LIGHT LENS COVER IS MISSING AT SEAT ROWS 24 AND 27. MAINTENANCE INSTALLED NEW OVERHEAD EMERGENCY LIGHT LENS COVERS FOR SEAT ROWS 24 AND 27 PER AMM 33-51. OK FOR SERVICE. (LP #8293852)
THE R1 DOOR SLIDE PRESSURE GAUGE INDICATION IS IN THE RED ZONE. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE SLIDE AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE REPLACED THE R1 DOOR SLIDE PER AMDS 2561-9005. COMPLETED RII STEPS PER AMDS 2561-9005 QC2047. (LP #2010939)
MULTIPLE WIRTEUPS FOR TAIL CONE CAM RIGGING. RAM 1. PLEASE REMOVE TAIL CONE AND INSPECT ALL ATTACH FITTINGS CABLES BRACKETS AND CAMS PER AMDS WORK CARD 5352-4013. 00-0000-3-0001. ADJUSTED TAILCONE RELEASE CAM REF B717 AMM 53-52-03. (LP #1935731)
THE TAILCONE RELEASE CAM IS CLOCKED WRONG. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY SEE NRC 001-0115:5352-4002/002 00349: ADJUSED TAILCONE RELEASE CAM REF B717 AMM 53-52-03. (LP #1934458)
THE CONDUIT FOR TAILCONE RELEASE CABLE IS DENTED, RT SIDE LOWER AREA (MARKED). THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY SEE NRC 001-0265:5300-2004/007 00082: REPLACED CONDUIT AND TAILCONE RELEASE CABLE REF BOEING DRAWING 5913350. (LP #1934205)
THE TAILCONE RELEASE CAM IS CLOCKED WRONG AND OUT OF ADJUSTMENT. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY NRC 001-0115:5352-4002/001 00303: ADJUSTED TAILCONE RELEASE MECHANISM CAM REF B717 AMM 53 -52-03. (LP #1927793)
THE EMERGENCY EXIT SIGN AT ROW 19 WOULD NOT LIGHT UP WHEN THE EMERGENCY LIGHTS WERE TURNED ON. MAINTENANCE REPLACED THE EMERGENCY BATTERY B5-120. OPERATIONAL CHECK WAS GOOD PER B717 AMM 33-51. OK FOR SERVICE. (LP #7374124)
ER/A 581113-14 REV A WAS ISSUED FOR DAMAGE AT STA 1037, L-14L. FOLLOW ON ACTION IS REQUIRED. ACCOMPLISH ER/A 581113-14 REV A, SECTION II WITHIN 3,500FC FOLLOWING THE COMPLETION OF SECTION I (ACCOMPLISHED AT 36,606FC). ASSOCIATED ER/A 95-581113 ADDED FOR AC 9507. C/W STEPS #1 AND #2 REF. ER/A 581113-14 REV. A. MEASURMENT OF REPAIR STRAP IS .600. C/W HFEC REF ERA 581113-14 REV. A SECTION 2 STEP 3. NO DEFECTS NOTED (QC 2005). C/W STEPS #4 AND #5 SECTION II ERA 581113-14 REVISION A. MONITOR,ER/A 581113-14 REV A WAS ISSUED FOR DAMAGE STATUS: TERMINATED DEFRL AUTHORITY TOPP: REFERENCE 95-581113. (LP #1778204)
ER/A 560974-14AD REV D ISSUED FOR REPAIRS TO LOWER FIXED LE ON VERTICAL STAB. ACCOMPLISH ER/A 560974-14AD REV D SECTION III REPEAT INSPECTIONS EVERY 3,000FC FOLLOWING THE ACCOMPLISHMENT OF SECTION II (ACCOMPLISHED AT 53,271HRS AND 36,606CYC). ASSOCIATED ER/A 95-560974 ADDED FOR AC 9507. REF ER/A 561912-14 REV C AND LP #1776790 FOR ALL REQUIRED FOLLOW ON ACTION. ASSOCIATED AA 5530-01048 ADDED FOR AC 9507. TERMINATED LOG PER LINE 4 COMMENTS AND ER/A 560974-14AD. CLOSED LOG AND REMOVED MONITOR INSP PER ALERT 27APR21 AND LOG COMMENT. (LP #1777434)
AIRCRAFT 9507, STABILIZERS / VERTICAL / APPROX. ZFS =62 - 44 / RH SPAR CAP, AND FORWARD SPAR WEB / CRACKS / AMOC 21-151. CORRECTIVE ACTION: COMPLIED WITH ER/A 561912-14AD SECTION III. (LP 1776790)
VERTICAL STABILIZER LH LOWER FIXED LEADING EDGE SKIN FASTENER HOLES / BUSHING REPAIR / AD RELATED. REF PREVIOUS LOG 1263304. ER/A 562080-14 REV C ISSUED AND IS CURRENT REVISION. SECT III INSPECTIONS TBA WITHIN 3000FC AFTER SECT II, AND AT EVERY 3000FC REPEATING THEREAFTER. FOLLOW ON ACTI ON IS REQUIRED. NDT IS REQUIRED FOR FOLLOW ON ACTION. ASSOCIATED ER/A 95-562080 ADDED FOR AC 9507. THIS LP MAY BE CLOSED. LP #1776790 / ERA 561912-14AD REV C CONTAINS ALL REQUIRED INSPECTIONS FOR ER/A 562080-14AD REV C. ASSOCIATED AA 5530-01048 ADDED FOR AC 9507. TERMINATED LOG PER LINE 3 COMMENTS AND ER/A 562080-14AD AND REMOVED MONITOR INSP PER ALERT 27APR21. (LP #1776877)
THE CEILING EMERGENCY LIGHTS IN THE FIRST CLASS CABIN TO ROW 14 ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY POWER SUPPLY B5-227 IAW B717 AMM 33-51. PERFORMED OPERATIONAL CHECK AND ALL LIGHTS CHECK GOOD.
CRACK ON RETAINER INTERNAL WINDOW SKIN RT SIDE OF COCKPIT AREA (SM). NRC 00720: RETAINER INTERNAL WINDOW SKIN RT SIDE OF COCKPIT AREA WAS REPAIRED PER ER/A 581231-14 REV ORIGINAL (SECTION I: PERMANENT REPAIR) AND ETI-17-19-172 REV 1 ASSOCIATED ER/A 14-581231 ADDED FOR AC 9507. (LP #1264452)
CORROSION ON SPLICE BTW STA 650 AND 660 LONGERON 30 C1 AREA (SM). NRC 00490: SPLICE BTW STA 650 AND 660 LONGERON 30 C1 WAS REPAIRED PER ETI-17-19-168 REV 2 AND ER/A 581203-14 REV ORIGINAL. ASSOCIATED ER/A 14-581203 ADDED FOR AC 9507. (LP #1263609)
CRACK ON AREA AND HOLES OF SETTLEMENT THE SUPPORT AT AFT UPPER CORNER OF COCKPIT RT SLINDING WINDOW CUT OUT (SM). NRC 00654: AFT UPPER CORNER OF COCKPIT RT SLINDING WINDOW CUT OUT WAS REPAIRED PER SRM 56-10-02-2R AND ER/A 581052-14 REV ORIGINAL ASSOCIATED ER/A 14-581052 ADDED FOR AC 9507. (LP #1263332)
ERA 560974-14AD REV C ISSUED FOR REPAIRS TO LOWER FIXED LE ON VE RTICAL STAB. DTA / DTE IS REQUIRED. ASSOCIATED AA 5530-01048 ADDED FOR AC 9507. ASSOCIATED ER/A 00-560974 ADDED FOR AC 9507. DTE HAS BEEN ACCOMPLISHED. FOLLOW ON INSPECTIONS ARE REQUIRED. SECTION III OF ER/A 560974-14AD REV D AND LOGPAGE 1777434 WILL TRACK THE INSPECTION REQUIREMENTS. THIS LOGPAGE CAN BE CLOSED. TERMINATED LOG PAGE PER ENGINEERING COMMENTS ON LINE 4. CLOSED LOG AND REMOVED MONITOR INSP PER ALERT 11APR21 AND LOG COMMENTS. (LP B#1262616)
CORROSION AT SEVERAL FILLET FAIRING RUBSTRIPS BTW STA Y=560 TO STA Y=848 AND STA Y=858 TO STA Y=917 BOTH SIDES (FUS). NRC 00520: CORROSION LEVEL 2, RUBSTRIPS (8 EA) BTW STA Y=560 TO STA Y=848 AND STA Y=858 TO STA Y=917 BOTH SIDES WERE REPLACED PER SRM 51-20-05-0G AND SRM 53-20-70-0I. (LP #1261392)
CRACK ON INTERNAL STRUCTURE OF L1 DOOR. NRC 0066: WEB ON INTERNAL STRUCTURE OF L1 DOOR WAS REPAIRED PER SRM 52-00-00-2R REPAIR 2 FIG 201. (LP #1260373)
PUNCTURES, MISSING INSERTS, AND DELAMINATION ON FLOOR PANEL #211ANF (CPIL). NRC 00702: PUNCTURES AND DELAMINATION ON FLOOR PANEL #211ANF WERE REPAIRED PER SRM 51-70-09-2R-6 PAR. A TO H. NEW INSERTS WERE INSTALLED PER AMM 20-60-11. (LP #1259314)
CORROSION IN ACCESSES #620DT, 620FT, 620DB, AND 620EB ON AREA SETTLEMENT AND COUNTERSINK AT FUEL TANK (AD). NRC 00551: CORROSION LEVEL 2, CORROSION IS OUT OF LIMITS. FUEL ACCESS PLATE #620EB WAS REPLACED. FUEL ACCESS PLATE WAS INSTALLED UNDER NR 2040-0012, JOB 001-0340. FUEL ACCESS PLATES #620DT AND 620FT WERE REPLACED AND INSTALLED UNDER NR 2040-0012, JOB 001-0340. FUEL ACCESS #620DB MUST BE ATTENDED UNDER LP #1259822. (LP #1259827)
CRACKED LT NOSE LANDING GEAR JAMB BEAM AROUND STA Y=52 (FYT). NRC 00607: CRACKED LT NOSE LANDING GEAR JAMB BEAM AROUND STA Y=52 WAS REPAIRED PER ETI-17-19-158 REV. 1 AND ER/A 581111-14 REV ORIGINAL SECTION I PERMANENT REPAIR. ASSOCIATED ER/A 14-581111 ADDED FOR AC 9507. (LP #1260161)
CRACK FRAME BTW STA 1037 AND L=13 RT (FUS). NRC 00618: FRAME BTW STA 1037 AND L=13 RT WAS REPAIRED PER ER/A 581116-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND ETI-17-19-160 REV 1. ASSOCIATED ER/A 00-581116 ADDED FOR AC 9507. (LP #1258837)
CRACK ON LT CUSP MEMBRANE STA 536 BTW X=44.5 AND X=54.5 AT PAX CABIN. (CPAX). NRC 00395: LT CUSP MEMBRANE STA 536 BTW X=44.5 AND X=54.5 WAS REPLACED PER 53-00-55-2R-4 FIG 226. (LP #1259207)
CRACK FRAME BTW STA 1037 AND L=14 ALSO L=17 LT (FUS). NRC 00617: FRAME BTW STA 1037 AND L=14 ALSO L=17 LT WAS REPAIRED PER ER/A 581057-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND ETI-17-19-159 REV.1. ASSOCIATED ER/A 00-581057 ADDED FOR AC 9507. (LP #1258551)
CRACKED RT NOSE LANDING GEAR JAMB BEAM AROUND STA Y=47 (FYT). NRC 00456: RT NOSE LANDING GEAR JAMB BEAM AROUND STA Y=47 WAS REPAIRED PER SRM 53-10-14-2R-2 FIG.201. (LP #1256460)
CORROSION ON BEARING HOUSING OF RUDDER TORQUE TUBE AFT FUSELAGE AREA (A&P). NRC 00586: CORROSION LEVEL 2, BEARING HOUSING OF RUDDER TORQUE TUBE AFT FUSELAGE AREA WAS REPLACED PER AMM 27-21-01 AND SRM 51-41-02-0G. (LP #1252777)
CORRROSION AT LWR, FWD DOOR JAMB. NRC 00170: CORROSION LEVEL 2, LOWER FWD DOOR JAMB WAS REPAIRED PER SRM 53-20-05-2R FIGURE 201. (LP #1250148)
CORROSION ON LT CUSP WEB MEMBRANE IS OUT OF LIMITS FROM STA Y=980 TO Y=983 AND BTW X=60 TO X=54 (CPAX). NRC 00664: CORROSION LEVEL 2, CUSP WEB MEMBRANE LT FROM STA Y=980 TO Y=983 AND BTW X=60 TO X=54 WAS REPAIRED PER SRM 53-00-55-2R-4 FIG. 215. (LP #1249804)
CRACK AT L=4 LT STA Y=1022 (CPAX). NRC 00532: L=4 LT STA Y=1022 WAS REPAIRED PER SRM 53-00-05-2R-2- FIG. 201. (LP #1248630)
CRACK AT LONGERON 5 LT, BS 1022. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R.
CORROSION IN ACCESSES #520CT AND 620CT ON AREA SETTLEMENT AND COUNTERSINK AT FUEL TANK (AI) (AD). NRC 00549: CORROSION LEVEL 2, FUEL ACCESS PLATE #520CT AND 620CT WERE REPLACED PER AMDS 2040-0012, 2040-0010, AND VERIFIED PER B717-200 IPC 57-22- 01-01. (LP #1243350)
CRACK AT FUSELAGE SKIN STA Y=1095 BTW L=13/14 LH (FUS). NRC 00039: FUSELAGE SKIN STA Y=1095 BTW L=13/14 LH WAS REPAIRED PER ER/A 580773-14 REV. ORIGINAL (PERMANENT REPAIR) AND ETI-17-19-155 REV. 1. WILL BE MONITORED BY LOG PAGE #1241544 PER ER/A NO 580773-14 REV. ORIGINAL. ASSOCIATED ER/A 14-580773 ADDED FOR AC 9507.
CRACK ON KEEL BEAM FORMER RH SIDE STA Y=715 AND X=-37. NRC 00595: CRACK ON KEEL BEAM FORMER RH SIDE STA Y=715 AND X=-37 WAS REPAIRED PER B717-200 SRM 51-70-11-2R-1 FIG. 201. (LP #1242493)
CRACK GUSSET AT L=7 RH STA Y=1022 (CPAX). NRC 00537: GUSSET AT L=7 RH STA Y=1022 WERE REPAIRED PER ER/A 580881-14 REV. ORIGINAL SECTION I: PERMANENT REPAIR AND ETI-17-19-154 REV. ORIGINAL. ASSOCIATED ER/A 14-580881 ADDED FOR AC 9507. (LP #1243761)
CRACK ON KEEL BEAM FORMER LH SIDE STA Y=696 AND X=30 (CPAX). NRC 00590: KEEL BEAM FORMER LH SIDE STA Y=696 AND X=30 WAS REPAIRED PER B717-200 SRM 51-70-11-2R-1 FIG 201. (LP #1243383)
CRACK AT L=6 LH STA Y=1022 (CPAX). NRC 00534: LONGERON 6 LH STA Y=1022 WAS REPAIRED PER B717-200 SRM 53-00-05-2R. (LP #1243376)
CRACK ON KEEL BEAM FORMER RH SIDE STA Y=679 AND X=-43 (FUS). NRC 00649: CRACK ON KEEL BEAM FORMER RH SIDE STA Y=679 AND X=-43 WAS REPAIRED PER B717-200 SRM 51-70-11-2R-1 FIG. 201. (LP #1241655)
CORROSION ON FLOOR SUPPORT STA X=07 FROM Y=160 TO Y=200 AT FWD WET AREA IN REF NRC 00587 (W1). NRC 00680: CORROSION LEVEL 2, FLOOR SUPPORT STA X=07 FROM Y=160 TO Y=200 AT FWD WET AREA (W1) WAS REPLACED PER B717- 200 SRM 53-10-51-0I-2 AND 51-41-01-0G. (LP #1240821)
CRACK ON KEEL BEAM FORMER RH SIDE STA Y=696 AND X=-30 (FUS). NRC 00591: CRACK ON KEEL BEAM FORMER RH SIDE STA Y=696 AND X=-30 CRACK ON KEEL BEAM FORMER RH SIDE STA Y=696 AND X=-30 WAS REPAIRED PER B717-200 SRM 51-70-11-2R-1 FIG. 201. (LP #1241629)
CORROSION ON FLOOR SUPPORT STA X=-05 FROM Y=200 TO Y=160 AT FWD WET AREA IN REF NRC 00588 (W1). NRC 00679: CORROSION LEVEL 2, FLOOR SUPPORT STA X=-05 FROM Y=200 TO Y=160 WAS REPLACED PER B717-200 SRM 53-10-51-0I -2 AND SRM 51-41-01-0G.
CRACK ON KEEL BEAM FORMER LH SIDE STA Y=679 AND X=43 (FUS). NRC 00648: CRACK ON KEEL BEAM FORMER LH SIDE STA Y=679 AND X=43 WAS REPAIRED PER B717-200 SRM 51-70-11 FIG 201 REP 1. (LP #1240605)
CRACK ON KEEL BEAM FORMER LH SIDE STA Y=715 AND X=37 (FUS). NRC 00594: CRACK ON KEEL BEAM FORMER LH SIDE STA Y=715 AND X=37 WAS REPAIRED PER B717-200 SRM 51-70-11 FIG 201 REP 1. (LP #1240592)
CRACK AT LONGERON 4R, BS 1022, THE LONGERON WAS REPAIR IAW SRM 53-00-05-2R-2, FIG 201.
SEVERAL DENTS ON LOWER AREA FWD FLAP MOVABLE VANE LEFT WING (AI). NRC 00247: LH WING FWD FLAP MOVABLE VANE WAS REPAIRED PER B 717-200 SRM 57-53-01-2R PROCEDURE 1 REPAIR 1 PARAGRAPH 4 FIGURE 202.
CRACK ON RH CUSP MEMBRANE STA 620 BTW X=- 44.5 AND X=-54.5 AT PAX CABIN. (CPAX). NRC 00396: RH CUSP MEMBRANE STA 620 BTW X=-44.5 AND X=-54.5 WERE REPAIRED PER B717-200 SRM 53-00-55-2R- 4 FIG. 215. (LP #1236084)
CRACK ON RH CUSP MEMBRANE STA 536 BTW X=- 44.5 AND X=-54.5 AT PAX CABIN. RH CUSP MEMBRANE STA 536 BTW X=-44.5 AND X=-54.5 WERE REPAIRED PER B717-200 SRM 53-00-55-2R- 4- FIG.219.
CRACK AT LH RING PAN FWR LOWER SECTION BTW STA Y=889. LH RING PAN FWR LOWER SECTION BTW STA Y=889 WAS REPAIRED PER B717-200 SRM 56-20-02-2R-1 FIG. 202.
CRACK AT LH RING PAN FWD LOWER SECTION BTW Y=636. LH RING PAN FWD LOWER SECTION BTW Y=636 WAS REPAIRED PER B717-200 SRM 56-20-02-2R-1- FIG. 202.
CRACK AT RH RING PAN AT STA Y=870. RH RING PAN AT STA Y=870 WAS REPAIRED PER B717-200 SRM 56-20-02-2R-1- FIG. 202.
CRACK AT LH RING PAN FWD LOWER SECTION BTW Y=794. LH RING PAN FWD LOWER SECTION BTW Y=794/ 813 WAS REPAIRED PER B-717-200 SRM 56-20-02-2R-1 FIG. 202.
CRACK CUTOUT ON AFT HINGE AT RH/LH FIXED NLG DOOR (FUS). NRC 00136: CRACK CUTOUT ON AFT HINGE AT RH/LH FIXED NLG DOOR WAS REPAIRED PER B717-200 SRM 53-10-01-2R PROCEDURE 11 FIG. 201. (LP #1229158)
THE CABIN CEILING EMERGENCY LIGHTS AT ROW 1 & 24 ARE INOPERATIVE. ONE LIGHT AT EACH LOCATION IS INOPERATIVE, LIGHTS ARE NOT ADJACENT. EACH WAS RELAMPED, BUT DID NOT CORRECT THE PROBLEM. THE LIGHTS WERE PLACED ON MEL 33-51-01A AND PLACARDS INSTALLED. MAINTENACE FOUND THAT THE EMERGENCY CEILING LIGHTS IN THE CABIN WERE DISCONNECTED. ONCE RECONNECTED THEIR OPERATION WAS GOOD AND THE AIRCRAFT IS OK FOR SERVICE. THE MEL WAS CLEARED AND THE PLACARDS REMOVED. (LP #5629262)
THE EMERGENCY EXIT COVER DIFFUSER LENS IS MISSING AT 29B. MAINTENANCE INSTALLED THE LENS COVER. CHECK IS GOOD. (LP #0918194)
SKIN AROUND LAV VENT ON BELLY BULDGED. FOUND AREA CORRODED AND SKIN CRACKED. REPAIRED IAW ER/A 566366-14, REV O.
THE RIGHT HAND FUSELAGE SKIN AT VACUUM WASTE TANK VENT STA 1022-1037 / L28R-29R HAS CORROSION. ER/A 566366-14 ISSUED AND IS CURRENT. SECTION II IS LIMITED TO 12 MONTHS AFTER SECTION I, PENDING DAMAGE TOLERANCE ANALYSIS. ASSOCIATED ER/A 95-566366 ADDED FOR AC 9507. (LP #0472945)
THE CAPTAIN REPORTED A FIRE IN THE CABIN AT THE L1 DOOR AND TAXIED THE AIRCRAFT BACK TO THE GATE. THE FLIGHT ATTENDANT USED THE FIRE EXTINGUISHER ON A BURNING NAPKIN IN THE OVERHEAD LIGHT FIXTURE. THE NAPKIN REMAINS WERE REMOVED BY THE FLIGHT ATTENDANT. MAINTENANCE REPLACED THE BULB AS A PRECAUTION, INSTALLED A MISSING LENS, AND REPLACED THE EXTINGUISHER. THE AIRCRAFT HAS RETURNED TO SERVICE.
VERTICAL STAB LEFT AND RIGHT SIDE ZFS 52.267 UPPER TWO ROWS FASTENERS 85 LOOSE AND ELONGATED HOLES. COMPLIED WITH PRI 560974-14AD REV. 0, REV. 1, AND REV. 2. REPAIRED REF ER/A 560974-14AD REV ORIG. COMPLIED WITH ER/A 560974-14AD REV A.
ER/A 561912-14AD SECTION I ISSUED FOR CRACK REPAIR ON VERTICAL STABILIZER FRONT SPAR RT CHORD AND WEB. AD 2016-09-05 AFFECTED. ASSOCIATED ER/A 00-561912 ADDED FOR AC 9507. ASSOCIATED AA 5530-01048 ADDED FOR AC 9507. REF NEW LP 1262502FOR DTA, THIS LP TERMINATED PER ENGINEERING COMMENTS ON LINE 7. (LP #0229833)
VERTICAL STABILIZER RIGHT FRONT SPAR CAP FORWARD FLANGE HAS CRACK INDICATIONS IN FIVE HOLES BELOW THE LEADING EDGE SKIN SPLICE ZFS=52.267. REPAIRED ER/A 561912-14AD, REV ORIGINAL.
VERTICAL STABILIZER LEADING EDGE SPAR CAP WEB CRACKED. REPAIRED REF ER/A 561912-14AD, REV ORIGINAL.
VERTICAL STAB, FOUND RIGHT SPAR CRACKED AT ZFS=52.267 REPAIRED IAW ER/A 561912-14AD REV ORIGINAL.
CORROSION 0N GALLEY FLOOR SUPPORT ANGLE LBL 52 BETWEEN STA. 168 AND 193. M. NR 000-0001:5300-0116/029 00165 REMOVED CORROSION REF B717 SRM 53-00-00-1A. INSTALLED NEW GALLEY FLOOR SUPPORT. (LP #0222753)
CORROSION ON GALLEY FLOOR AT GALLEY SERVICE DOOR AFT GIRT BAR LATCH ATTACH FITTING. . REPLACED THE GIRT BAR ATTACH FITTING IAW SRM 51-00-07.
CORROSION ON GALLEY FLOOR AT GALLEY SERVICE DOOR FWD. GIRT BAR LATCH ATTACH FITTING. REMOVED AND REPLACED THE GIRT BAR ATTACH FITTING IAW SRM 51-00-07.
CORROSION ON GALLEY FLOOD ATTACH ANGLE LBL 44 BETWEEN BS 172 AND 199. REMOVED CORROSION IAW STM 53-00-00-1A. INSTALLED A NEW GALLEY FLOOR ATTACH ANGLE.
FOUND CABLE BALL ASSEMBLY DISCONNECTED FROM SLIDE HANDLE LATCH ASSEMBLY ON TAILCONE SLIDE. THIS IS CONSIDERED A DEFECT IN THE EMERGENCY ESCAPE SYSTEM AND COULD HAVE AN ADVERSE EFFECT ON THE EVACUATION ROUTE IF IT PREVENTED PROPER DEPLOYMENT OF THE TAILCONE. THIS IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE RE-SECURED THE CABLE ASSEMBLY IN REFERENCE TO AMDS WORKCARD 2561-9006 STEP 9.
EMERGENCY EXIT SIGN IN CEILING FORWARD OF 1ST CLASS IS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY IN B5-259 POWER PACK REF AMM 33-51. OPERATIONAL CHECK IS GOOD.
DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING IN THE TAIL COMPARTMENT WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPERATIONAL CHECK WAS GOOD.
DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTS IN ROWS 22-24 OF THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECK WAS GOOD.
DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGNS AT BOTH OF THE OVERWING HATCHES AND AT THE L2 DOOR WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPS CONDITION.
R1 EMER EXIT LIGHT MISSING BULB. RELAMPED LIGHT IAW AMM.
LEFT AFT OVERWING EMER LIGHT BULB INOPERATIVE. RELAMPED LIGHT IAW AMM.
TAIL COMPARTMENT CATWALK 3RD EMER LIGHT BULB INOPERATIVE. RELAMPED LIGHT IAW AMM.
TAIL COMPARTMENT HANDRAIL EMER LIGHT BULB INOPERATIVE. RELAMPED LIGHT IAW AMM.
LEFT DOOR OVERWING FWD EMER LIGHT BULB INOPERATIVE. RELAMPED LIGHT IAW AMM.
RIGHT DOOR OVERWING AFT EMER LIGHT BULB INOPERATIVE. RELAMPED LIGHT IAW AMM 33-51-00.
RIGHT OVERHEAD CEILING PANEL EMER LIGHT INOPERATIVE, BETWEEN ROW 22 - 23. RECONNECTED CONNECTOR IAW AMM.
EXTERIOR EMER OVERWING LIGHTS INOPERATIVE. R & R POWER SUPPLY IAW AMM.
LEFT TOP AFT OVERWING EXIT SIGN INOPERATIVE. R & R BATTERY PACK IAW AMM.
RIGHT TOP AFT OVERWING EXIT SIGN INOPERATIVE. R & R BATTERY PACK IAW AMM.
EMERGENCY LIGHT POWER SUPPLY B5-235 INOPERATIVE. R & R POWER SUPPLY IAW AMM.
RIGHT CUSP WEB CRACKED, BETWEEN BS 370 - 389. REPAIRED CUSP WEB IAW SRM.
LEFT CUSP WEB CORRODED, BETWEEN BS 351 - 370. REPAIRED CUSP WEB IAW SRM.
LEFT CUSP WEB CORRODED, BETWEEN BS 370 - 389. REPAIRED CUSP WEB IAW SRM.
SHEAR TIE CORRODED AT BS 1002. R & R SHEAR TIE IAW SRM.
RIGHT CUSP WEB CRACKED, BETWEEN BS 954 - 965. REPAIRED CUSP WEB IAW EA.
LEFT SIDE CUSP WEB CRACKED, BETWEEN BS 636 - 655. REPAIRED CUSP WEB IAW SRM.
RIGHT CUSP WEB CRACKED, BETWEEN BS 813 - 837. R & R CUSP WEB IAW DWG & SRM.
RIGHT CUSP WEB CORRODED, BETWEEN BS 851 - 870. REPAIRED CUSP WEB IAW SRM.
RIGHT CUSP WEB CORRODED, BETWEEN BS 870 - 889. REPAIRED CUSP WEB IAW SRM & EA.
RIGHT CUSP WEB CORRODED, BETWEEN BS 598 - 636. R & R CUSP WEB IAW SRM & DWG.
LEFT CUSP WEB CORRODED, BETWEEN BS 794 - 813, & LBL 55 - 60. R & R CUSP WEB IAW SRM.
RIGHT CUSP WEB CORRODED, BETWEEN BS 579 - 598. R & R CUSP WEB IAW SRM & DWG.
LEFT CUSP WEB CORRODED, BETWEEN BS 756 - 794, BETWEEN LBL 55 - 60. R & R CUSP WEB IAW SRM & DWG.
LEFT CUSP WEB CORRODED, BETWEEN BS 794 - 832, BETWEEN LBL 55 - 60. REPAIRED CUSP WEB IAW SRM & DWG.
CABIN SEAT TRACK BETWEEN BS 927 TO 1022, LBL 2. R & R SEAT TRACK IAW SRM & DWG.
CABIN SEAT TRACK CORRODED BETWEEN BS 851 TO 927, LBL 22. R & R SEAT TRACK IAW SRM & DWG.
CABIN SEAT TRACK CORRODED BETWEEN BS 503 - 589, RBL 22. R & R SEAT TRACK IAW SRM & DWG.
LEFT CUSP WEB CORRODED, BETWEEN BS 715 - 796, BETWEEN LBL 55 - 60. R & R CUSP WEB IAW SRM.
CUSP WEB CORRODED, BETWEEN BS 809 - 908 & RBL 55 - 60. R & R CUSP WEB IAW SRM & DWG.
RIGHT CUSP WEB CORRODED, BETWEEN BS 908 - 946. R & R CUSP WEB IAW SRM & DWG.
SEAT TRACK CORRODED, BETWEEN BS 899 - 1022, RBL 22. R & R SEAT TRACK IAW SRM.
SEAT TRACK CORRODED, BETWEEN BS 832 - 898, RBL 22. R & R SEAT TRACK IAW SRM.
LEFT CUSP WEB CORRODED, BETWEEN BS 313 - 389. REPAIRED CUSP WEB IAW SRM.
SEAT TRACK CORRODED, BETWEEN BS 823 - 898, RBL 44. R & R SEAT TRACK IAW SRM.
SEAT TRACK CORRODED, BETWEEN BS 653 - 832, RBL 22. R & R SEAT TRACK IAW SRM.
SEAT TRACK CORRODED, BETWEEN BS 589 - 646, RBL 44. R & R SEAT TRACK IAW SRM.
SEAT TRACK CORRODED, BETWEEN BS 588 - 646, RBL 22. R & R SEAT TRACK IAW SRM.
LEFT CUSP WEB CORRODED, BETWEEN BS 908 - 946, LBL 60. R & R CUSP WEB IAW SRM & DWG.
LEFT CUSP WEB CORRODED, BETWEEN BS 832 - 908, BETWEEN LBL 55 - 60. R & R CUSP WEB IAW SRM.
CUSP WEB CORRODED, BETWEEN BS 389 - 503, BETWEEN RBL 55 - 60. R & R CUSP WEB IAW SRM & DWG.
CUSP WEB CORRODED, BETWEEN BS 503 - 579, BETWEEN RBL 55 - 60. R & R CUSP WEB IAW SRM & DWG.
CABIN SEAT TRACK CORRODED, BETWEEN BS 446 - 503, RBL 44. R & R SEAT TRACK IAW SRM.
RIGHT CUSP WEB CORRODED, BETWEEN BS 715 - 756, BETWEEN RBL 55 - 60. R & R CUSP WEB IAW SRM & DWG.
RIGHT CUSP WEB CORRODED, BETWEEN BS 832 - 851, RBL 60. REPAIRED CUSP WEB IAW SRM & EA.
LEFT CUSP WEB CORRODED, BETWEEN BS 237 - 313, BETWEEN LBL 55 - 60. REPAIRED CUSP WEB IAW SRM.
LEFT CUSP WEB CORRODED, BETWEEN BS 503 - 560 & BETWEEN LBL 55 - 60. R & R CUSP WEB IAW SRM & DWG.
CABIN SEAT TRACK CORRODED, BETWEEN BS 556 TO 580, LBL 22. R & R SEAT TRACK IAW SRM & DWG.
SEAT TRACK CORRODED, BETWEEN BS 256 - 351, LBL 44. R & R SEAT TRACK IAW SRM.
SEAT TRACK CORRODED, BETWEEN BS 588 - 646, LBL 44. R & R SEAT TRACK IAW SRM.
CABIN SEAT TRACK CORRODED, BETWEEN BS 715 - 794, LBL 44. R & R SEAT TRACK IAW SRM.
CABIN SEAT TRACK CORRODED BETWEEN BS 580 TO 646, LBL 22. R & R SEAT TRACK IAW SRM & DWG.
CABIN SEAT TRACK CORRODED BETWEEN BS 715 TO 794, LBL 22. R & R SEAT TRACK IAW SRM & DWG.
C1 DOOR PAN UPPER WEB FLOOR SUPPORT CORRODED. R & R SUPPORT IAW SRM & DWG.
FRAME CORRODED AT BS 974, BETWEEN LONGERON 29R - 28L. REPAIRED FRAME IAW SRM.
LONGERON CORRODED, BETWEEN BS 927 - 974, LONGERON 30. REPAIRED LONGERON IAW SRM.
SHEAR TIE CORRODED AT BS 946, BETWEEN LONGERON 28L - 29R. R & R SHEAR TIE IAW SRM & DWG.
LONGERON CORRODED, BETWEEN BS 974 - 994, LONGERON 30. R & R LONGERON IAW SRM & DWG.
LONGERON CORRODED BETWEEN BS 889 - 1002, LONGERON 30. R & R LONGERON IAW SRM & DWG.
SUPPORT FRAME INTERCOSTAL CRACKED AT BS 813. R & R INTERCOSTAL IAW SRM & DWG.
FLOORBOARD SUPPORT CORRODED, BETWEEN BS 160 - 200, RBL 44. R & R SUPPORT IAW SRM & DWG.
CABIN FLOORBOARD SUPPORT CORRODED, BETWEEN BS 160 TO BS 200, LBL 44. R & R SUPPORT IAW SRM & DWG.
CABIN FLOORBOARD SUPPORT CORRODED AT BS 200, BETWEEN LBL 44 TO 18. R & R SUPPORT IAW SRM & DWG.
CABIN FLOORBOARD SUPPORT CORRODED, BETWEEN BS 196 - 200, LBL 14. R & R SUPPORT IAW DWG & SRM.
CABIN FLOORBOARD SUPPORT CORRODED AT BS 218, BETWEEN LBL 14 TO RBL 10. REPAIRED SUPPORT IAW SRM.
CABIN FLOORBOARD SUPPORT CORRODED, BETWEEN BS 160 TO 200, LBL 55. R & R SUPPORT IAW SRM & DWG.
CABIN SHORT FLOORBOARD SUPPORT, CORRODED AT BS 200, BETWEEN LBL 11 - 7. EVALUATED FLOOR SUPPORT IAW SRM & DWG.
FLOORBOARD SUPPORT, CORRODED AT BS 200, BETWEEN RBL 8 - 45. R & R SUPPORT IAW SRM & DWG.
AFT CARGO COMPARTMENT DOOR, JAMB PAN FRAME CORRODED AT BS 954, BETWEEN LONGERON 26R - 27R. REPAIRED PAN IAW SRM & EA.
DOOR JAMB FRAME, SKIN CORRODED AT BS 994, BETWEEN LONGERON 26R - 27R. REPAIRED SKIN IAW SRM.
FORWARD CARGO COMPARTMENT DOOR JAMB FRAME, CORRODED AT BS 427, LOWER LATCH. REPAIRED JAMB IAW EA.
R1 DOOR EMER EVAC SLIDE AFT GIRT BAR, SUPPORT FITTING CORRODED. R & R FITTING IAW SRM & DWG.
R1 DOOR EMER EVAC SLIDE, FWD GIRT BAR SUPPORT FITTING CORRODED. R & R FITTING IAW SRM & DWG.
FORWARD CABIN OVERHEAD CEILING EMER EXIT SIGN LENS CRACKED. R & R LENS IAW AMM.
AFT CABIN EXIT DOOR OVERHEAD EMER EXIT SIGN LENS CRACKED. R & R LENS IAW AMM.
FORWARD CARGO DOOR, JAMB LOWER PAN CORRODED. R & R PAN IAW SRM.
APPROACHING AIRPORT NOTICED AN IMBALANCE OF 900LBS LT TANK LOW. R & R O RING IAW MM.
R1 DOOR SLIDE COVER DETACHED AT UPPER HINGE. R & R COVER IAW MM.
R1 DOOR SLIDE COVER DETACHED. R & R COVER IAW MM.
CABIN OVERHEAD AFT EMERGENCY EXIT SIGN LENS MISSING. INSTALLED SIGN IAW MM.
FWD LOWER FLASHLIGHT INOPERATIVE. R & R BATTERY IAW AMM.
FWD EMERGENCY FLASHLIGHT INOPERATIVE. R & R BATTERY IAW AMM.
DIVERSION RT ENGINE OIL QUANTITY DROPPED TO 3 IN FLIGHT. THERE WAS NOTICEABLE OIL FUEL ODOR IN CABIN. SECURED OIL SCAVENGE TUBE & OIL VENT TUBE IAW MM.
RT EEPLS WIRE OUT OF POSITION AT ROW 27. REPAIRED WIRE IAW SWPM.
RIGHT EEPLS INOP BETWEEN ROW 20 TO ROW 24. R & R BATTERY POWER SUPPLY ASSY IAW AMM.
OVERHEAD EMERGENCY EXIT LIGHT ASSY IN FWD CABIN PLASTIC LENS TURNED UP MISSING DURING FLT. REINSTALLED LENS PER MM.
LEFT FWD EMERGENCY EXIT DOOR FWD BAYONET CUP CRACKED. REMOVED AND REPLACED LEFT FWD EMERGENCY EXIT DOOR FWD BAYONET CUP P/N D060277U5 PO 22125146 IAW B717 SRM 51-40-02.
FORWARD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER AMM.
ON FINAL APPROACH PUT GEAR DOWN DIDN'T GET ANY GREEN LIGHTS. CYCLED GEAR AND GEAR CAME DOWN FINE WITH THREE GREEN LIGHTS. REMOVED AND REPLACED PSEU PER AMM.
"HYD R QTY LO" ALERT IN FLIGHT. QTY WAS RESTORED WITH PUMPS OFF BUT ALERT CAME BACK ON WITH PUMPS ON. LANDED WITH MANUAL GEAR EXTENSION AND DOORS OPEN. REMOVED AND REPLACED MLG TRANSFER CYL REF AMM 32-33 + TEE ASSY TRANSFER CYL. REF 20-10 NO LEAKS NOTED AT THIS TIME OP'S CHECK GOOD AT THIS TIME.
L-1 EMERGENCY SLIDE DEPLOYED, DID NOT INFLATE. REMOVED AND REPLACED L-1 DOOR SLIDE REF MM 25-61-01.
EMERGENCY POWER FOUND ON,- BATTERIES DEPLETED. RECHARGED BATTERIES WITH EXTERNAL POWER AND OPS CHECKED WITHOUT FAULTS REF AMM 24-34.
RT FUSELAGE SKIN, 3 DENTS LOCATED AFT OF R-1 DOOR BETWEEN L-16R AND 18R. CUT OUT DAMAGED SKIN SECTION FROM STATION 185 TO 229, BETWEEN L-16R AND 18R. FABRICATED AND INSTALLED NEW SKIN SECTION USING .050" 2024-T3, AND REPAIR DOUBLERS .063" 2024-T3, DOUBLER .025" 2024-T3 AND SPLICE DOUBLER .032" TI 4V-AL. REFERENCE B717 SRM 53-00-01, REPAIR 6 AND AIRTRAN EA 17-53-02668B SECTION 4.
AFT PRESSURE BULKHEAD FWD FACE STA 1053 HAS CENTER DOUBLER CORRODED. REMOVED AND REPLACED DOUBLER ON AFT PRESSURE BULKHEAD STA 1053 PER REF B717 SRM 51-41-02 AND 51-41-05.
LT ALTERNATE STATIC PORT CRITICAL AREA HAS A DENT STA 236.5 BELOW PORT 2 INCHES FWD TO 4 INCHES AFT. REMOVED AND REPLACED STATIC PORT PLATE, THIS CONDITION CAUSED DENT AT LT ALTERNATE STATIC PORT (PLATE FOUND CORRODED).
AFT PRESSURE BULKHEAD FWD FACE STA 1053 LONG 30 LOWER ANGLE P/N 9915561-73 CORRODED. REMOVED AND REPLACED CORRODED ANGLE P/N 9915561-73 PER REF B717 SRM 51-41-05.
CEILING EMERGENCY LIGHT L2-742 DOES NOT ILLUMINATE. RE-TERMINATED CONNECTOR P1-6717/R5-6717 IAW SWPM 20-31-17. PERFORMED OPS CHECK OF EMERGENCY LIGHT SYSTEM IAW AMM 33-51-00, AND OPS CHECK NORMAL.
ON CLIMBOUT, RIGHT QUANTITY LOW LEVEL 2 ALERT ILLUMINATED FOLLOWED BY COMPLETE LOSS OF FLUID, AND RIGHT HYDRAULIC PRESSURE LOW LEVEL 2 ALERT. FOUND BOTH MLG DOORS DAMAGED, AND HYDRAULIC TRANSFER CYLINDER CRACK OBSERVED AT END OF CASTING. REPLACED BOTH MLG DOORS, AND HYDRAULIC TRANSFER CYLINDER REF MM 32-14, AND 29-22. OPS AND LEAK CHECK GOOD.
L1 DOOR SLIDE RELEASE CABLE PULLED THROUGH SLIDE ASSEMBLY EYE-LET HOLES. REMOVED AND REPLACED L1 DOOR EVAC SLIDE ASSY. OK FOR SERVICE, REF 25-61 AMM.
R1 DOOR SLIDE COVER SEPARATED FROM DOOR. REPLACED R1 DOOR SLIDE COVER ASSY IAW MM 25-61. OK FOR SERVICE.
EMERGENCY AISLE LIGHTS INOP, ROW 20 THRU 25. REPLACED B5 -119 CHASSIS, OPS GOOD PER AMM 33-51.
MAIN CABIN SEAT TRACK HAS CORROSION BETWEEN STA 204 AND 256 RBL 22. REMOVED SECTION OF SEAT TRACK FROM STA 198 TO STA 301.5 AND INSTALLED NEW SECTION PER DC9/MD80 SRM 53-05 FIG 4F7001 AND EA 17-53-02053IR.
FUSELAGE STRUCTURE INTERNAL WEB CRACKED AT STA 208 LONG 11L. TRIM OUT DAMAGED AREA AND INSTALLED TYPICAL WEB REPAIR PER SRM 51-40-02.
FUSELAGE STRUCTURE INTERNAL WEB CRACKED AT STA 208 LONG 15L. TRIM OUT DAMAGED AREA AND INSTALLED TYPICAL WEB REPAIR PER SRM 51-40-02.
EO 17-5310-2937 AFT LEFT STA 1178 CANTED FRAME INSPECTION IDENTIFIED CONFIGURATION 2 CONDITION 5. ACCOMPLISHED REPAIR TO AFT FUSELAGE FRAME CAP, CANTED STA 1178.225, LEFT SIDE IAW AIRTRAN TASK CARD 17-5310-2980.
EO 17-5310-2895 AFT RIGHT STA 1178 CANTED FRAME INSPECTION IDENTIFIED CONFIGURATION 2 CONDITION 5. ACCOMPLISHED REPAIR TO AFT FUSELAGE FRAME CAP, CANTED STA 1178.225, RIGHT SIDE IAW AIRTRAN TASK CARD 17-5310-2990.
MAIN CABIN SUB FLOOR (SHEAR WEB) BS 198 RBL 45 HAS CORROSION. INSTALLED WEB REPAIR REF B717 SRM 51-70-10 AND 51-40-02.
MAIN CABIN FLOOR SUPPORT BETWEEN BS 146 AND BS 200 LBL 7 HAS CORROSION ON CLIP NUT ATTACHMENT HOLES. REMOVED AND REPLACED CABIN FLOOR SUPPORT TRACK PER B717 SRM 51-41-01.
MAIN CABIN FLOOR SUPPORT BETWEEN BS 157 AND BS 218 RBL 2 HAS CORROSION. REMOVED AND REPLACED CABIN FLOOR SUPPORT PER B717 SRM 51-41-01.
MAIN CABIN SUB FLOOR (SHEAR WEB) BETWEEN BS 202 AND BS 218 RBL 22 HAS CORROSION. REMOVED FASTENER, REMOVED CORROSION OUT OF LIMIT, CUT DAMAGED ARES, INSTALLED WEB REPAIR REF B717 SRM 51-40-02.
MAIN CABIN FLOOR SUPPORT BS 198 BETWEEN LBL 5 AND RBL 5 HAS CORROSION. REMOVED AND REPLACED CABIN FLOOR SUPPORT PER B717 AMM 51-10-04 AND SRM 51-10-04, 51-41-02.
MAIN CABIN FLOOR SUPPORT BETWEEN BS 202 AND BS 218 RBL 11 HAS CORROSION. REMOVED AND REPLACED CABIN FLOOR SUPPORT PER B717 SRM 51-41-02.
MAIN CABIN FLOOR SUPPORT BETWEEN BS 204 AND BS 256 LBL 15 HAS CORROSION. REMOVED AND REPLACED CABIN FLOOR SUPPORT PER B717 SRM 51-41-02.
MAIN CABIN FLOOR SUPPORT FS 237 BL 0 HAS CORROSION. REMOVED AND REPLACED CABIN FLOOR SUPPORT PER B717 SRM 51-41-05.
ON DESCENT LOST RT GEN TRIED ONE RESET - STARTED APU BUS AC BUS TIE WOULD NOT CLOSE. REMOVED AND REPLACED RT PCDU, GEN CONTROL RELAY & EXT PWR MAIN BTR REF AMM 24-21. APU BUS, OPS CHECK GOOD.
ARRIVED ON PLANE 2125Z. STANDBY LIGHTS ON. PLANE ARRIVED ON GATE AT 1900Z. REMOVED AND REPLACED EMERGENCY PWR PACKS AS PER M/M 33-51.
E-PATH LIGHTS & OVERWING EXIT SIGNS (LOWER) INOP FROM ROW 20 TO ROW 24. INSTALLED SERVICEABLE EMER LIGHT POWER SUPPLY & BATTERY AT RIGHT ROW 25 IAW AMM 33-51-03. OPS CHECK GOOD.
FWD CARGO DOOR THRESHOLD CORRODED BEYOND LIMITS. REPLACED THRESHOLD PAN IAW B717 SRM 53-20-15.
FIRST OFFICER'S I/B SEAT TRACK CORRODED BEYOND LIMITS. REPLACED SEAT TRACK, FABRICATED FROM RAW STOCK.
FOUND DENT ON A/C 708 RIGHT SIDE FUSELAGE AT STATION 160 BETWEEN L24 AND L25 DENT MEASURED .141 X 1.5 X 1.4. INSTALLED DOUBLER REPAIR AND FILLER AT RT SIDE FUSELAGE AT STA 160 BETWEEN L24 AND L25.
FIRST CLASS EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT POWER IAW AMM 31-51 OPS CK OK.
EMERGENCY PATH LIGHT 1FWD, 10, AND 20 INOP. RELAMPED, OPS CHECK NORMAL. REF MM 33-00.
FUSELAGE DENT FWD OF STATION 256 ABOVE STR 18 L. D=2.0 X .075. FOUND TO BE WITHIN LIMITS PER B717 SRM 53-00-01 CONDITION 2. REQS REPETITIVE INSP AT C-CHECK INTERVALS. INSTALLED SKIN REPAIR AT FUSELAGE AT FWD OF STA 256 ABOVE STR 18L IAW AND B717 SRM 53-00-01 FIG 201. MATERIAL USED 2024 T3 .050, 35.5 X 14 INCH FOR FINGER, 2024 T3.025 FOR DOUBLER AND 2024 T3 .050, 35.5 X 4 INCH.
RT ENGINE SYSTEM FAIL, LOW RPM, SHUT DOWN. REMOVED AND REPLACED RT FMC AND RT EEC IN ACCORDANCE WITH AIRCRAFT MAINTENANCE MANUAL 73-23 AND 73-21. PERFORMED HIGH POWER RUN, OPS CHECK GOOD.
FOUND DENT AT BS 275 AFT OF R1 DOOR. INSTALLED REPAIR DOUBLER AND FILLER IAW RES 01-004.
DURING FLIGHT, SMOKE WAS OBSERVED COMING OUT OF AREA OF FUEL PUMP SWITCHES ON UPPER COCKPIT PANEL. FOUND LOGO LIGHT SWITCH NOT WORKING. PULLED PUSH BUTTON OUT AND FOUND ONE BULB BURNT INTO SOCKET WITH SIGNS AND SMELL OF SMOKE AROUND IT. PULLED CIRCUIT BREAKER AND DEFERRED LOGO LIGHT PER MEL.
FMC RANGE DISAGREE, NO ALTIMETERS ONLY FLIGHT INSTRUMENTS WERE AIRSPEED AND ATTITUDE. FLIGHT CONTROL PANEL BLANK. TROUBLESHOT SYSTEM ELECT SYNOPTIC PAGE REVEALED RT PCDU AT FAULT. ALSO CONFERRED WITH BOEING, AGREED THAT R/HG PCDU FAILURE CAUSED THIS PROBLEM. REMOVED AND REPLACED PCDU IAW MM 24-21-04-000-803. SYSTEM OPS CHECKED NORMAL.
FOUND ROW 11 EMERGENCY PATH LIGHT INOPERATIVE, PINCHED BETWEEN SEAT AND SEAT TRACK. SPLICED NEW WIRE IAW B717 MPS 1465 AND STANDARD WIRING MANUAL 20-10-03.