N899AT
Registered owner: DELTA AIR LINES INC, GA (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| DELTA AIR LINES, INC. (DALA) | Operator | 2024-04-03 – 2024-04-03 | Operator named in NTSB report |
| DELTA AIR LINES INC | Operator | 2024-04-03 – 2024-04-03 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
ATB/TIRE- THE CREW PERFORMED AN AIR TURN BACK DUE TO A BLOWN TIRE ON ROTATION WITH ASSOCIATED LEFT ENGINE VIBRATIONS. REPLACED #1- AND #2-WHEEL ASSY. FLAP AND ENGINE REPAIR IN PROGRESS. (8687069) (AIRCRAFT GROUNDED)
CREW DIVERTED TO ORD AFTER RECEIVING A LT SYSTEM HYDRAULIC QUANTITY LOW MESSAGE WITH QUANTITY DEPLETING. FOUND LEFT HYD LEAKING AT HYD RESERVOIR BLEED VALVE DRAIN HOSE CONNECTION. REPLACED RESERVOIR. LEAK CHECK NORMAL.(7712608)
SHIP 9557 -ATB- PERFORMED AN AIR TURN BACK TO ATL DUE TO RIGHT ENGINE SYSTEM FAIL MESSAGE JUST AFTER TAKEOFF. CORRECTIVE ACTION: DURING INSPECTION OF RIGHT ENGINE TGT THERMOCOUPLE PROBES, FOUND TCC COOLING TUBE LINE BLOWN OUT AND MISSING HARDWARE. REPLACED COOLING TUBE AND HARDWARE. (LP 6976664, 1024228)
SHIP 9557 STRONG ELECTRICAL ODOR ON FINAL RIGHT S THE GEAR WENT DOWN AND FLAPS WENT TO 18 DEGREES. R/R TRANSFORMERS TI-5 AND T1-6.(T1-5 SMELLED BURNT) PER B717 SWPM 20-20-03. RT NOSE LDG AND TAXI LIGHT CKS OK. C/B FUNCTION NORMAL. REF B717 WDM 34-41-01 (7262952)
ENROUTE F/O WINDSHIELD WAS ARCING. FOLLOWED BY A "LEVEL 1 WSHLD HEAT FAIL" MESSAGE. RAN QRH CHECK LED US TO "WINDSHIELD CRACKED OR ARCING" CHECKLIST ON PAGE 3.13. PULLED CB Z-24. LOOKS LIKE A HAIRLINE CRACK ON OUTER PANE - UPPER PORTION OF WINDSHIELD. MAINTENANCE REPLACED F/O SIDE WINDOW REF B717 AMM 56-11-02. SPEED TAPE APPLIED TO ALLOW CURE ON SEALANT SEE LP 9992705. (LP #9992704)
BOTH AFT EMERGENCY DOORS "EMERGENCY EXIT IDENTIFIER" LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHTS BATTERY PACK POWER SUPPLY B5-119 PER B717 AMM 33-51-03. OPERATIONAL TEST WAS GOOD. (LP #5908832)
THE AFT LEFT AND AFT RIGHT OVERWING EXIT LIGHTS (LOWER) ARE INOPERATIVE. DISCONNECTED R5-4255A FOR T/S. RE-CONNECTED R5-4255A AND REPLACED BATTERY POWER SUPPLY AND BATTERY ASSEMBLY B5-119 PER B717 AMM 33-51. ALL CHECKS ARE GOOD.
BOTH FCC FAULTING BOTH REDUNDANT STOP SWITCHES ON DESCENT MULTIPLE FLIGHTS. VERIFY CONDITION AND SECURITY OF REDUNDANT RUDDER LIMITER RETURN SPRINGS. FOUND RUDDER LIMITER PUH ROD BINDING. REMOVED ROD AND REPLACED BOTH BEARINGS REF P.S. 900-9-1 #06. INSTALLRD ROD REF B717 AMM 27-26. FUNCTIONAL TEST OF RUDDER LIMITER TEST NORMAL. INSTALLATION, RIG, & TEST OK. SELECTED SDR -YES- FROM -NO- PER AMT 882284. (LP #0319513)
LT MLG UPPER STRUT O/B ATTACH LUG HAS CORROSION ON THE AFT FACE. MARKED. SUMMARY SEE NRC 004-0003:3211-4001/015 00016: C/W ERA 615978-14 REV ORIGINAL. VERIFIED PRI AND ERA MATCH. (LP #0209458)
LT MLG - TRAPEZOIDAL FITTING BUSHING PITTED ON AFT SIDE. MARKED IN RED. SUMMARY SEE NRC 004-0003:3211-4001/014 00015: REPLACED BUSHING PER OHM 57-40-1. (LP #0206822)
TRUNNION MOUNT ATTACH AFT FITTING AFT LUG AFT BUSHING HAS CORROSION. (MARKED) REF NR 013 VISIT ID P682670620231227 AND REPAIRED PER B717 SRM 51-10-04. (LP #0205683)
EMERGENCY EXIT SIGNS AT LOCATION 601 ARE INOPERATIVE. THE INTERIOR EMERGECY EXIT LIGHTS ARE FLASHING IN FLIGHT. MAINTENANCE REPLACED B5-235 POWER SUPPLY AND BATTERY IAW B717 AMM 33-51. OPERATIONAL TESTS WERE GOOD. (LP #0112909)
THE EMERGENCY EXIT LIGHTS BY L1 DOOR ABOVE F/A JUMPSEAT ARE INOPERATIVE. MAINTENANCE DROPPED THE O2 MASK DOOR BELOW LIGHT FOR BETTER ACCESS. PERFORMED OPERATIONAL TEST OF THE EMERGENCY LIGHTING SYSTEM IAW B717 AMM 33-51. TWO OUT OF THREE LIGHT ASSEMBLYS FROM POWER SUPPLY B5-235 OPERATIONAL. REPLACED POWER SUPPLY B5-235 IAW B717 AMM 33-51. OPERATIONAL TEST PASSED. AIRCRAFT OK FOR SERVICE. (LP #5512733)
CORROSION ON R1 DOOR SERVICE LOWER DOOR JAMB STA Y=168 TO STA Y=200. IN REFERENCE NRC 0428. PTAS. SUMMARY OF NRC 00531: CORROSION LEVEL 2, R1 DOOR SERVICE LOWER DOOR JAMB STA Y=168 TO STA Y=200 WAS REPAIRED PER PRI 609065-14 REV 2 AND ER/A 609065-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-609065 ADDED FOR AC 9557. (LP #2818514)
CORROSION ON DOOR JAMB AFT LOWER SECTION STA =950 TO STA=992. SUMMARY OF NRC 00071: CORROSION LEVEL 2. DOOR JAMB AFT LOWER SECTION STA=950 TO STA=992 WAS REPAIRED PER B717-200 SRM 53-20-15-2R PROCEDURE 7 REPAIR 7. (LP #2816939)
CORROSION ON FLOOR PANELS 121HF, 181KF, 181HF, 181UF, 121DF, 121FF, 121NF, 181AF (PART 2), 181FF, 181AF (PART 3), 181CF, 121TF, 181JF, 181DF, 121SF, 121JF, 121CF, 121PF, 121QF, 121MF, 121UF, 121VF, 121SF, 181AF (PART 1), 181EF (PART 1), 181EF (PART 2), AND 181BF. SUMMARY OF NRC 00380: CORROSION LEVEL 2. CORROSION ON FLOOR PANELS WAS REMOVED PER B717-200 SRM 51-10-04-0G PAR 26 C FLOOR PANELS 121DF, 121FF, 121TF, 121JF, 121CF, 121PF, 121MF, 121UF, 181AF (PART 1), 181KF, 181UF, 181FF, 181CF, 181JF, 181DF, 181EF (PART 1 & 2), AND 181BF WERE EVALUATED WHITIN LIMITS PER B717-200 SRM 53-00-00- 1A ALLOWABLE DAMAGE GENERAL PARAGRAPH 4. C. FIGURE 103 AND FLOOR PANEL 121VF, 121SF, 181AF (PART 2), AND 121HF WERE FABRICATE PER B717-200 ER/A 544901-14 REV A AND INSTALLED UNDER JOB 001-0003 AND JOB 001-0123. ALSO, FLOOR PANEL 121QF, 181HF, 121NF, AND 181AF (PART 3) WERE REPLACED WITH NRC 00379. ASSOCIATED ER/A 14-544901 ADDED FOR AC 9557. (LP #2818160)
CORROSION ON FLOOR SUPPORT BTW STA Y=120 AND Y=148 X=-50 AT COCKPIT. SUMMARY OF NRC 00440: CORROSION LEVEL 2. FLOOR SUPPORT BTW STA Y=120 TO Y=148 X=-50 AT COCKPIT WAS REPLACED PER B717-200 SRM 51-41-08-0G. (LP #2814601)
CRACKED MEMBRANE BTW STA Y=172 AND Y=187 APROX AND X54 AT CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00577: MEMBRANE BTW STA Y=172 AND Y=200 APROX AND X54 AT CABIN FLOOR STRUCTURE WAS REPLACED PER DRAWING 9936534-5 REV BW AND PER B717-200 SRM 51-41-05-0G AND 51-41-02-0G. (LP #2813658)
CORROSION ON FLOOR SUPPORT STA Y=215 TO 157 X54, X44, X7, X-7, X-44, X-54, X-55 CPAX (W1). SUMMARY OF NRC 00409: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=215 TO 157 X54, X44, X7, X-7, X-44, X-54, X-55 CPAX (W1) WERE REPLACED PER DWG 9936534 REV BW AND PER B717-200 SRM 51-41-05-0G AND 51-41-02-0G. (LP #2811469)
CORRODED OUT OF LIMITS IN REF TO NRC 339: CORROSION ON FLOOR SUPPORT BTW STA 200 AND -X=46 TO -X=57 AT PAX CAB. SUMMARY OF NRC 00584: NEW FLOOR SUPPORT BTW STA 200 AND -X=46 TO -X=57 WAS INSTALLED, ADJUSTED, AND DRILLED PER B717-200 SRM 51-40-08- 0G GENERAL AND DWG: 9936535 REV. CS. (LP #2809556)
CORROSION ON WEB FROM STA Y 155 TO 200 AND FROM X 20 TO X-60 AT R1 DOOR LOWER DOOR JAMB. IN REF NRC 00531. SUMMARY OF NRC 00549: CORROSION LEVEL 2. WEB FROM STA Y 155 TO 200 AND FROM X 20 TO X-60 AT WAS REPLACED PER B717-200 SRM 51-41 -02-0G AND 51-41-05-0G. (LP #2808481)
CORROSION ON WEB FROM STA 218 TO 237, X -55 TO 44:5 AT W1 IN REF NRC 531. CPAX. SUMMARY OF NRC 00546: CORROSION LEVEL 2. WEB FROM STA 218 TO 237, X -55 TO 44:5 AT W1 WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4 FIG 226 AND SRM 51-41-02-0G. (LP #2805008)
ERODED MATERIAL ON FUSELAGE SKIN BTW STA 992 AND LONGERON 25R APPROX (DOOR CUTOUT). SUMMARY OF NRC 00214: FUSELAGE SKIN BTW STA 992 AND LONGERON 25R APPROX (DOOR CUTOUT) WAS REPAIRED PER B717-200 SRM 53-20-15-2R PROCEDURE 12 REPAIR 12 PAR 6 OPTION 1, FIGURE 201. MAINTENANCE REQUERIMENTS WERE VERIFIED AND FOLLOWING ACTION ARE NEEDED: PERFORM THE INITIAL VISUAL INSPECTION WITHIN 8000 FLIGHT CYCLES, THEN PERFORM REPETITIVE VISUAL INSPECTIONS EVERY 8000 FLIGHT CYCLES, AND REPLACEMENT IS NOT APPLICABLE PER B717-200 SRM 53-20-15-2R PROCEDURE 12 REPAIR 12 PAR 7 A. TABLE 202. (LP #2803966)
CRACK FRAME OF LH AFT LAVATORY ENGINE PYLON SUPPORT BULKHEAD, STA 1022 AND LONGERON 7 LH. SUMMARY OF NRC 00231: FRAME OF LH AFT LAVATORY ENGINE PYLON SUPPORT BULKHEAD, STA 1022 AND LONGERON 7 LH WAS REPAIRED PER PRI 608989-14 REV. 0 AND ER/A 608989-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-608989 ADDED FOR AC 9557. (LP #2803577)
CORROSION ON WEB PRODUCTION DOUBLER FROM STA 157 TO 178 AT R1 DOOR LOWER JAMB. W1. SUMMARY OF NRC 00550: CORROSION LEVEL 2. WEB PRODUCTION DOUBLER FROM STA 157 TO 178 AT R1 DOOR LOWER JAMB W1 WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #2803318)
DELAMINATION AND BROKEN COMPOSITE MATERIAL AND SHEET ON FWD CARGO FLOOR PANEL 121CF AND 121NF (C1). SUMMARY OF NRC 00376: FWD CARGO FLOOR PANEL 121CF AND 121NF WERE MANUFACTURED PER ERA 544901-14 REV A PAR 6. AND FIGURE 5 AND ERA 591778-14TR REV ORIGINAL SECTION I PERMANENT REPAIR. ASSOCIATED ER/A 14-544901 ADDED FOR AC 9557. (LP #2794128)
CRACK ON FRAME STA 1037 BTW LONG-16 LH TO LONG-17 AT PAX CABIN. SUMMARY OF NRC 00534: FRAME STA 1037 BTW LONG-16 LH TO LONG-17 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 4, REPAIR 4. (LP #2794265)
CORROSION ON PREVIOUS DOUBLERS REPAIR OF RH CUSP WEB BTW STA Y=446 TO Y=503, STA Y=541 TO Y=560, AND Y=598 TO Y=617 AT PAX CABIN. SUMMARY OF NRC 00460: CORROSION LEVEL 2. PREVIOUS DOUBLERS REPAIR OF RH CUSP WEB BTW STA Y=446 TO Y=503, STA Y=541 TO Y=560, AND Y=598 TO Y=617 WERE REPLACED PER B717 SRM 53-00-55-2R-4. (LP #2790339)
CORROSION ON PREVIOUS DOUBLER REPAIR OF LH CUSP WEB BTW STA Y=446 TO Y=465 AND STA Y=484 TO Y=503 AT PAX CABIN. SUMMARY OF NRC 00459: CORROSION LEVEL 2. PREVIOUS DOUBLER REPAIR OF LH CUSP WEB BTW STA Y=446 TO Y=465 AND STA Y=484 TO Y=503 AT PAX CABIN WERE REPLACED PER B717 SRM 53-00-55-2R-4. (LP 32790495)
CORROSION ON LH CUSP MEMBRANE (WEB) UPPER FACE BTW STA 863 TO 865 AT PAX CABIN. SUMMARY OF NRC 00545: CORROSION LEVEL 2. CUSP MEMBRANE (WEB) UPPER FACE BTW STA 863 TO 865 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #2790489)
CORROSION ON SEAL RETAINER (2 EA) ON THE LOWER CUTOUT AREA AT FWD CARGO COMPARTMENT DOOR. SUMMARY OF NRC 00079: CORROSION LEVEL 2. SEAL RETAINERS (2 EA) ON THE LOWER CUTOUT AREA AT FWD CARGO COMPARTMENT DOOR WERE FABRICATED PER DWG #PL 5910141 REV FE AND REPLACED PER B717-200 SRM 51-41-01-0G. (LP #2787889)
CRACK INNER PAN AFT FRAME, BEAM #1 END AT FWD CARGO DOOR C1. SUMMARY OF NRC 000168: INNER PAN AFT FRAME, BEAM #1 END AT FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R REPAIR 1, FIGURE 201. (LP #2787424)
CORROSION ON RH CUSP MEMBRANE (WEB) UPPER/ LOWER SURFACE FROM STA 200 TO 218 AT PAX CABIN. SUMMARY OF NRC 00564. CORROSION LEVEL 2: RH CUSP MEMBRANE (WEB) FROM STA 200 TO 218 AT PAX CABIN WAS REPLACED PER B717-200 SRM 53-10-51-0I PROCEDURE 2 ITEM 32. (LP #2787225)
CORROSION ON LOWER HALF OF SETTLEMENT AREA ON RUDDER DRIVE TORQUE (FUSELAGE STRUCTURE). SUMMARY OF NRC 00373: PLATE ASSY, BEARING SUPPORT WAS REPLACED PER B-717-200 SRM 51-41-02-0G AND 51-41-01-0G. (LP #2787763)
CORROSION ON FLOOR SUPPORT STA Y=256 X-22 TO X10 CPAX (W1). SUMMARY OF NRC 406: FLOOR SUPPORT STA Y=256 X-22 TO X10 CPAX WAS REPLACED PER B717-200 SRM 51-41-05-0G. (LP #2785801)
CRACK ON CUTOUT DOOR STRUCTURE FWD SIDE ON LOWER CORNER, BTW BEAMS 1-2 AT FWD CARGO DOOR. SUMMARY OF NRC 00076: CUTOUT DOOR STRUCTURE FWD SIDE ON LOWER CORNER, BTW BEAMS 1-2 AT FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 4, REPAIR 4. (LP #2786046)
CORROSION OUT OF LIMITS ON LH OTBD SEAT TRACK BTW STA 357 TO 358, 427 TO 428, AND 462 TO 463. PER B717-200 SRM 53-20-52-1A PROCEDURE 1 ALLOWABLE DAMAGE 1 PARAGRAPH 4. A. FIGURE 101 AND DWG S00482. SUMMARY OF NRC 00530: CORROSION LEVEL 2. LH OTBD SEAT TRACK BTW STA 357 TO 358, 427 TO 428, AND 462 TO 463 WERE REPAIRED PER B717-200 SRM 53-20-52-2R PROCEDURE 1 REPAIR 1 AND SRM 51-41-01-0G. (LP #2785150)
BROKEN PAN ON FWD CARGO DOOR AFT SIDE BTW 1-2 BEAMS. SUMMARY OF NRC 00091: PAN OF FWD CARGO DOOR AFT SIDE BTW 1-2 BEAMS WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 4, REPAIR 4. (LP #2783956)
DURING RT OVERWING FRAME INSPECTION, FOUND FRAME AT STA 696 CRACKED. RT OVERWING FRAME AT STA 696 REPLACED ON CARD 5310-01436-03B.
UPPER RADIUS OF THE FRAME TAB AT STA Y=696.00 RT OVERWING FRAME HAS CRACK INDICATION. INSTALLED INTERCOSTALS 11R, 12R, 10R, 15R, 16R, 17R, AND 18R REF DWG 9919671. REPAIRED ON WORK CARD 5310-01436-03B.
FWD CARGO DOOR CUT-OUT INNER PAN HAS AREAS OF CORROSION. REPAIRED IN REF TO SRM 53-20-15-2R PROC 6.
FOUND DAMAGE ON THE LT INBD FLAP TRAILING EDGE WEDGE. PERFORMED A TEMP REPAIR IAW ER/A 568347-14.
CABIN STANDBY LIGHT AT SEAT 15 ABC MISSING THE LENS. REPLACED THE OVERHEAD EMERGENCY LIGHT ASSY IAW AMM 33-51. PERFORMED AN OPS TEST IAW AMM 33-51. OPS TESTED OK.
SKIN CRACKED BS 1152 BETWEEN STRINGERS 2 & 3R. REPAIRED THE SKIN IAW ER/A 549622-14 REV O.
FUSELAGE SKIN CRACKED BS 1152 BETWEEN STR 3L & 4L AT FORMER I/B FASTENER. HFEC VERIFIED IAW NDTSPM ETHF PROCEDURE 1, 06-10-01 .001. FABRICATED DOUBLER AND FILLER. REPAIRED IAW SRM 53-02-01 FIG 202.
FOUND CORROSION AT BS 1022 AT LONGERON 29R TO 29L AFT CARGO. BLENDED AREAS OF CORROSION ON AFT SIDE OF FRAME 1022 FROM STR 29R TO 29L IAW B717 SRM 53-00-00 FIG 103. MINIMUM OF .033 REMAINING OF ORIGINAL .050 AT STR30, FOUND TO BE OUT OF LIMITS IAW B717 SRM 53-00-00 FIG 103 REPAIRED FRAME IAW B717 SRM 53-20-03 REPAIR 3 TAG 6785. (LP #2713262)
FRAME CORRODED AT BS 598, STRINGERS 29 & 30R. REPAIRED THE FRAME IAW SRM 53-20-07 REPAIR 3 FIG 201.
LEFT INBD SEAT TRACK LBL 22 CORRODED BS 756 TO 794. BLENDED OUT OF LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 53-20-52 R5 FIG 201, AND SRM 51-41-05.
FRAME CORRODED BS 465, STRINGERS 29 & 30R. CORROSION BLENDED IAW SRM 53-00-00 FIG 103 0.036 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00 FIG 103. REPAIRED IAW SRM 53-20-07 REPAIR 3.
FRAME CORROSION, STA 522 AFT LWR AT STR 30. CORROSION ON FRAME AT STA 522, LONGERON 30 BLENDED IAW SRM 53-00-00 FIG 103. 0.010" MATERIAL FOUND REMAINING, FOUND OUT OF LIMITS IAW SRM 53-00-00 FIG 103. REPAIRED IAW SRM 53-20-07 FIG 201 REPAIR 2.
SKIN DENTED AT BS 215 BETWEEN STRINGERS 15 AND 16L. REPAIRED IAW ER/A 529431-REV A.
FRAME CORROSION, STA 484 AFT LWR AT STR 30. BLENDED CORROSION AT STA 484 STR 30 ON FRAME AND FOUND TO BE OUT OF LIMITS ORIG 0.050 REMAINING 0.029". REPAIRED FRAME IAW SRM 53-20-07 REPAIR NR 3 FIG 201.
FRAME CORROSION, STA 275 AFT LWR AT STR 30 & 29L. BLENDED CORROSION AT STA 256 STR 29L, MATERIAL REMOVED .016 FOUND TO BE OUT OF LIMITS. COMPLETED FRAME REPAIR IAW SRM 53-20-07 REPAIR 3 PG 214 FIG 201.
SEAT TRACK AT RBL 22 STA 822-1022 FOUND TO BE OUT OF LIMITS DUE TO CORROSION. REQUIRES REPAIR. REPLACED SEAT TRACK FROM STA 822-1022 RBL 22 PER SRM 51-40-08 PG 1 PARA 3 & SRM 51-4105 PG 1.
STA 1022 BULKHEAD FWD SIDE, FORMER BELOW STR 6R CRACKED. REPLACED FORMER AT STA 1022 L6R IAW SRM 51-41-02, FABRICATED FORMER FROM 2014-T6 .050 IAW DWG PL9912243.
BS 927 TO 994 LONGERON 30 HAS MANY AREAS OF CORROSION. CLEANED UP CORROSION IAW SRM 53-00-00 FIG 103. REPLACED THE LONGERON IAW SRM 53-20-05 REPAIR 1.
SEAT TRACK RBL 22 BS 822-1022, FOUND TO BE OUT OF LIMITS DUE TO CORROSION. REPLACED THE SEAT TRACK IAW SRM 51-40-08 PG 1 PARA 3 & SRM 51-41-05 PG 1.
SEAT TRACK FOUND TO BE CORRODED OUT OF LIMITS AT RBL 44.5 STA 427-600. REQUIRES REPAIR. REPAIRED CORRODED SEAT TRACK SECTION BETWEEN RBL 44.5 STA 427-600 IAW SRM 53-20-52 REPAIR 5.
SEAT TRACK FOUND TO BE CORRODED OUT OF LIMITS AT RBL 22 STA 351-607. REQUIRES REPAIR. REPAIRED SEAT TRACK CORROSION FROM STA 351-607 RBL 22 IAW SRM 53-20-52 REPAIR 5.
RT CTR SEAT TRACK RBL 44.5 HAS CORROSION BETWEEN BS 889-954. BLENDED CORROSION ON SEAT TRACK AND FOUND TO BE OUT OF LIMITS IAW SRM 53-20-52 FIG 101. REPLACED IAW SRM 53-20-52 REPAIR 5.
CUSP WEB CRACKED AT BS 674 LBL 44.5 LEFT. REPAIRED THE CUSP WEB IAW SRM 53-00-55 REPAIR 4.
AFT CARGO BS 851, BL 0 FLOOR SUPPORT AFT END CRACKED. REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02 PG 1.
NR 1 ENGINE APRON HAS AREA OF CHAFING ABOVE AFT MOUNT AND CRACK AND GOUGE BELOW AFT MOUNT. NR 1 ENGINE APRON HAS AREA OF CHAFING AND CRACK AND GOUGE APPLIED NEW EDGE IAW SRM 54-00-00 FIG 1 AND REPAIRED IAW SRM 54-00-00 REPAIR 1 PG 201.
LEFT INBD SEAT TRACK LBL 22 HAS CORROSION AROUND NUTCLIP HOLES FROM BS 756 TO 794. BLENDED OUT OF LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 53-20-52 R5 FIG 201, SRM 51-41-05.
FRAME FORMER ANGLE AT AFT SIDE OF 1022 BULKHEAD AT LONGERON 14L IS CRACKED. REPLACED AFT FORMER ANGLE STA 1022, L14L PN 9912243V199, IAW SRM 51-41-22 AND 51-41-05.
FRAME FORMER ANGLE AT AFT SIDE OF 1022 BULKHEAD AT LONGERON 14R IS CRACKED. REPLACED DAMAGED FORMER AT STA 1022, LONGERON 14R IAW SRM 51-40-2, 51-40-05.
UPPER SURFACE OF THE CENTER TANK, LT SIDE OF ACFT, STA 737, LBL 43 SEAT TRACK SUPPORT IS CRACKED 2 PLACES, MARKED. REPLACED SEAT TRACK SUPPORT AT STA 737, LBL 43 IAW SRM 51-41-05, PG 17, STEP 8.
LEFT CENTER SEAT TRACK, BL44.5L IS CORRODED AND GOUGED IN SEVERAL PLACES, FROM STA 256 TO STA 351. REPAIRED LT CENTER SEAT TRACK BL 44.5, STA 319 IAW SRM 53-20-52, REPAIR 1.
LEFT CENTER SEAT TRACK, BL44.5L IS CORRODED AND GOUGED IN SEVERAL PLACES, FROM STA 541 TO STA 636. LEFT CTR SEAT TRACK WAS CORRODED AND GOUGED IN SEVERAL PLACES FOUND TO BE OUT OF LIMITS AT STA 636. REMOVED .055" REMAINING .045" OUT OF LIMITS IAW SRM 53-20-52. REPLACED SEAT TRACK FROM STA 586-636 MATERIAL 1D EXTRUSION TAG 1685633, PART 500484-7050-T76511 IAW SRM 53-20-52, REPAIR 5, PAGE 2 FABRICATED AND DRILLED TRACK IAW SRM 53-20-52, REPAIR 5, PRIMED SEAT TRACK IAW PSM 900-3-6, NR 3. TOP COATED IAW PSM 900-3-6, NR 3 INSTALLED SEAT TRACK IAW SRM 51-41-05, GAUGE TAG 2737.
RIGHT CTR SEAT TRACK, BL 44.5 HAS CORROSION BETWEEN STA 813- STA 820. REPAIRED RT CTR SEAT TRACK, BL 44.5, STA 809 IAW SRM 53-20-52, REPAIR 1.
STA 1022 BULKHEAD FWD SIDE, FORMER BELOW STR 16L CRACKED. REPLACED FWD FORMER PN 99122430189, AT STA 1022 BELOW S162 IAW SRM 51-41-02 AND 51-41-05.
CRACK ON INTERCOSTAL ANGLE IN CEILING IN FLC STA 636. LOCATION MARKED. REPAIRED CRACKED INTERCOSTAL IAW SRM 53-00-00, REPAIR 1, FIG 201.
RIGHT OTBD CUSP WEB IS CRACKED ON INBD EDGE AT STA 579. REPAIRED RT OTBD WEB AT INBD EDGE OF STA 579R IAW SRM 53-00-55, REPAIR 4 FROM 7075-T6-020 FILLER AND 7075-T6, .032 DOUBLER FILLER AND DOUBLER ALODINED PRIMED IAW SRM 51-22-01, PAGES 2 AND 3.
MAINTENANCE FOUND THE L1 DOOR EMERGENCY ESCAPE SLIDE PINS PULLED OUT. THE L1 DOOR SLIDE WAS REPLACED.
DURING SPECIAL VISIT, OVERWING FRAME INSPECTION,FOUND FRAME CRACKED AT BS 715 RT UPPER RADIUS OF FRAME TAB. REPLACED OVERWING FRAME IAW AMDS WC 5310-1436-03B AND COMPLETED REQUIRED INSPECTIONS.
FLOORBEAM CRACKED BS 737, RBL 54. INSTALLED A NEW FLOOR BEAM IAW SRM 51-40-02 & 51-40-05.
VERTICAL STIFFENER BS 737, RBL 44 BELOW SEAT TRACK FOUND CRACKED. INSTALLED STIFFENER SUPPORT ANGLE SRM 51-40-05.
DURING SERVICE CHECK, FOUND EMERGENCY LIGHTS INOPERATIVE FROM F/A PANEL. REPLACED AFT CARGO EMERGENCY LIGHTS POWER SUPPLY IAW AMM 33-51. CKS GOOD.
RETURNED TO DEPARTURE DUE TO THE LOSS OF THE LT HYDRAULIC PRESSURE & QUANTITY. LOCATED LEAK AT AT LT ENGINE DRIVEN PUMP PRESSURE LINE PN 7972127-554. SUPPORT CLAMP CHAFED THROUGH LINE. REPLACED LINE, BRACKET AND CLAMPS. THE ACFT HAS RETURNED TO SERVICE.
DURING FUNCTIONAL TEST OF TAIL CONE RELEASE SYSTEM, FOUND LOCK CABLE TO BE OUT OF ADJUSTMENT AS REQUIRED IAW AMM 53-52-01-720, STEP F, E, 5 ADJUSTED IAW 53-52-01. COMPLETED FUNCTIONAL CHECK. OPS CKS GOOD. RII COMPLETE.
DURING HYDRAUIC TROUBLESHOOTING IN THE TAIL CONE AREA, MAINTENANCE NOTICED THE TAIL CONE RELEASE CABLE MISROUTED AND RUBBING ON STRUCTURE. REROUTED CABLES IAW AMM 53-52-01, FIG'S 503 AND 504. LOCK CABLE AND PULL CABLE HAD NO TURNBUCKLES BROKEN OR TENSIONS DISTURBED.
TAIL COMPARTMENT EMER LIGHTS BULB INOPERATIVE. RELAMPED LIGHT IAW AMM.
TAIL COMPARTMENT PLASTIC EMER EXIT SIGN AROUND PULL HANDLE CRACKED. R & R SIGN IAW AMM.
TAIL CONE SLIDE LANYARD FRAYED. R & R LANYARD IAW AMM.
MID CABIN CEILING PANEL OVERWING DOORS EMER EXIT SIGN LENS CRACKED. R & R LENS IAW AMM.
RIGHT WING TO BODY FORMER CORRODED AT BS 832. R & R FORMER IAW SRM.
WING TO BODY FAIRING SPLICE ATTACHED TO FORMER CORRODED AT BS 851. R & R SPLICE IAW SRM.
MAIN CABIN FLOOR PANEL 222 QF DELAMINATED. R & R PANEL IAW SRM.
MAIN CABIN FLOOR PANEL 223 DF DELAMINATED. R & R BOARD IAW SRM.
MAIN CABIN FLOOR PANEL 222 ADF DAMAGED. R & R BOARD IAW SRM.
MAIN CABIN FLOOR PANEL 222 YF DAMAGED. R & R BOARD IAW SRM.
MAIN CABIN FLOOR PANEL 222TF DELAMINATED. R & R BOARD IAW SRM.
MAIN CABIN FLOOR PANEL 222 UF DELAMINATED. R & R BOARD IAW SRM.
MAIN CABIN FLOOR PANEL 222 LF DELAMINATED. R & R BOARD IAW SRM.
MAIN CABIN FLOOR PANEL 222 AHF DELAMINATED. R & R BOARD IAW SRM.
MAIN CABIN FLOOR PANEL 222 AGF DELAMINATED. R & R BOARD IAW SRM.
MAIN CABIN FLOOR PANEL 222 AVF DELAMINATED. R & R PANEL IAW SRM.
CUSP WEB CORRODED BETWEEN BS 484 TO 490 RBL 54. REPAIRED CUSP WEB IAW SRM.
CUSP WEB CORRODED BETWEEN BS 541 TO 560 RBL 60. REPAIRED CUSP WEB IAW SRM.
CUSP WEB CORRODED BETWEEN BS 465 TO 484 RBL 54. REPAIRED CUSP WEB IAW SRM.
CUSP WEB CORRODED BETWEEN BS 446 TO 465 LBL 54. REPAIRED CUSP WEB IAW SRM.
SPLICE DOUBLER CORRODED AT BS 588 RBL 54. R & R DOUBLER IAW SRM & DWG.
LEFT CUSP WEB CRACKED AT BS 799. R & R CUSP WEB IAW SRM & DWG.
CUSP WEB CORRODED BETWEEN BS 794 TO 813 RBL 54. REPAIRED CUSP WEB IAW SRM.
CUSP WEB CORRODED BETWEEN BS 696 TO 715 RBL 54. REPAIRED CUSP WEB IAW SRM.
CUSP WEB CORRODED BETWEEN BS 697 TO 598 RBL 54. REPAIRED CUSP WEB IAW SRM.
CUSP WEB CORRODED AT BS 605 LBL 54. REPAIRED CUSP WEB IAW SRM.
CUSP WEB CORRODED BETWEEN BS 484 TO 503 LBL 54. REPAIRED CUSP WEB IAW SRM.
SEAT TRACK CUSP WEB CORRODED AT BS 898 RBL 54. REPAIRED CUSP WEB IAW SRM & DWG.
SEAT TRACK CUSP WEB CORRODED AT BS 563 RBL 54. REPAIRED CUSP WEB IAW SRM.
SEAT TRACK CUSP WEB CORRODED AT BS 571 LBL 54. REPAIRED CUSP WEB IAW SRM.
SEAT TRACK CUSP WEB CORRODED BETWEEN BS 465 TO 484 LBL 54. REPAIRED CUSP WEB IAW SRM.
SEAT TRACK CUSP WEB CORRODED BETWEEN BS 525 TO 530, LBL 54. REPAIRED CUSP WEB IAW SRM.
FORWARD CARGO DOOR JAMB ANGLE CORRODED BETWEEN BS 390 TO 410. R & R ANGLE IAW SRM & DWG.
STRINGER CRACKED AT BS 1120 LONGERON 1R. REPAIRED STRINGER IAW SRM.
LEFT MLG WW DOOR INNER SKIN CRACKED AT OTBD FWD EDGE. REPAIRED SKIN IAW SRM.
RT EMERGENCY LIGHT COVER MISSING AT ROW 2. INSTALLED COVER IAW SIP.
AFT EMERGENCY EXIT LIGHT POWER SUPPLY COVER LOOSE. SECURED COVER IAW AMM
LEFT WING TO BODY FAIRING 1505L AFT LOWER RUB STRIP CORRODED. REMOVED AND REPLACED RUB STRIP PER SRM.
C-1 DOOR FWD SEAT TRACK SUPPORT BRACKET CRACKED AT BS 370. REMOVED & REPLACED BRACKET IAW SRM.
RIGHT WING TO BODY FAIRING NR 160 & RUB STRIP CORRODED BETWEEN BS 908 TO BS 946. REMOVED AND REPLACED RUB STRIP IAW SRM.
R1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTINGS CORRODED. REMOVED & REPLACED FITTING IAW SRM.
FRAME CORRODED AT BS 908, BETWEEN L30-L29L. REMOVED AND REPLACED FRAME IAW SRM.
FRAME CORRODED AT BS 927, BETWEEN L30-L29L. REMOVED AND REPLACED FRAME IAW SRM.
FRAME CORRODED AT BS 889, BETWEEN L30-L28L. REMOVED AND REPLACED FRAME IAW SRM.
FRAME CORRODED AT BS 974, BETWEEN LONGERON 29L - 29R. REMOVED AND REPLACED FRAME IAW SRM.
FRAME STRAP CORRODED AT BS 954, LONGERON 28L. REMOVED AND REPLACED STRAP IAW SRM.
EMERGENCY LIGHT COVER MISSING AT 2ND ROW OF LIGHTS. RE-INSTALLED LENS COVER PER MM.
DURING ARRIVAL CHECK CAPTAIN PUSHED LEFT GROUND FLOODLIGHT IN AND SMOKE STARTED COMING OUT FROM BEHIND THE SWITCH. FOUND LEFT GROUND FLOOR CIRCUIT BREAKER POPPED. REMOVED AND REPLACED SWITCH PER MM.
FWD LOWER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.
EMERGENCY LIGHT LENS COVER MISSING OVER ROW 10. REPLACED LENS.
MISSING ONE LENS COVER FOR EMERGENCY LIGHT SYSTEM IN CEILING ABOVE ROW 29. INSTALLED SERVICEABLE LENS COVER REF 33-51.
EMERGENCY EXIT LIGHT LENS COVER OVER AFT F/A JUMPSEAT FELL OFF AND CRACKED. WILL NOT STAY ON. INSTALLED LENS AT AFT F/A STA SP8103.
E/E COMPARTMENT CEILING CABIN FLOOR WEB, STA 200, BL 0, CORROSION. ACCOMPLISHED CABIN FLOOR WEB DOUBLER REPAIR PER B717 SRM 51-10-04, 53-00-00 AND 51-70-10.
STANDBY LIGHT COVER MISSING. REPLACED COVER.
L1 PACK PRESSURE APPEARS OUTSIDE OF GREEN. REMOVED AND REPLACED L1 DOOR SLIDE ASSY IAW MM 25-61. AIRCRAFT OK FOR SERVICE.
AFT CARGO DOOR CUTOUT LOWER PAN AREA HAS CORROSION FORWARD AND AFT SECTION. CUT OUT DAMAGED SECTION OF LOWER PAN BETWEEN STA 954 AND 994, INSTALLED NEW SECTION PER REF B717 SRM 53-20-15.
ON DEPARTURE, FIRE DETECTOR LEFT ENGINE FAIL ILLUMINATED AT 12,000 FEET, WENT OUT AT ABOUT 13,000 FEET FOLLOWED BY A LEFT ENGINE FIRE INDICATION. INDICATION WENT OUT WHEN THROTTLE WAS MOVED TO IDLE. OVERWEIGHT LANDING APPROX 106,500 LBS. FOUND BORESCOPE PLUG 'F' ON NR 1 ENGINE LOOSE. RESECURED PLUG PER MM 72-33. PERFORMED FIM 26-11, TASK 807. NO DEFECTS NOTED. A/C LANDED BELOW OVERWEIGHT LANDING LIMIT OF 110,000 LBS. A/C OK FOR SERVICE REF MM 05-51-04, 1B.
L1 EMERGENCY SLIDE APPEARS LOOSE. REMOVED AND REPLACED L1 DOOR SLIDE REF AMM 25-61.