N369NB
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 | 2017-03-06 – 2017-03-06 | Operator named in NTSB report |
| DELTA AIR LINES INC | Operator | 2017-03-06 – 2017-03-06 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
SCRATCHED CREW OXYGEN MASK OBSERVER POSITION ON COCKPIT. REMOVED CREW OXYGEN MASK POSITION 3RD OCCUPANT ON COCKPIT ON UNSERVICEABLE CONDITION IAW AMM 35-12-41-000-002A STEP 4. . REPLACED CREW OXYGEN MASK OBSERVER POSITION ON COCKPIT IAW FAM AMM 35-12-41-000-002-A & IAW FAM AMM35-12-41- 400-002-A. (LP: 1664160, AIRCRAFT WAS GROUNDED).
DURING M2 AND WHILE INSPECTING PER 5316-01052-05B THE HORIZONTAL STIFFENER OF LATERAL WINDOW FR4 RHS WAS FOUND COMPLETELY REMOVED DUE TO PREVIOUS REWORK PER THIS ER/A ORIGINAL REVISION. PER SECTION IV OF 573692-14 REV B, ACCOMPLISH SECTION IV REPETITIVE INSPECTION WITHIN EVERY 2,200 FC FROM SECTION III (17JUN26). ASSOCIATED ER/A 31-573692 ADDED FOR AC 3169. (LP: 1651940, AIRCRAFT WAS GROUNDED)
CORROSION STRINGER 38RH FROM FR59 TO FR60 IN AFT CARGO COMPARTMENT (SS I: 534150). REPLACED STRINGER SECTION 38RH BTW FR 59 TO FR 63 IN AFT CARGO COMPARTMENT AS PER A319 SRM 51-42-11, A319 SRM 51-72-11 AND DRAWING E53476330 ISSUE AD, RELEASE DATE 11/JUL/18, MEASUREMENTS OF CORROSION ON STRINGER ARE: L=10.416 IN W=0.718 IN D=0.004IN. SEE INDIVIDUAL SIGN OFF ORNRC #143/100 RII INSPECTION COMPLETE. (LP: 1632157, AIRCRAFT WAS GROUNDED)
LEVEL 2 CORROSION, CORROSION SPIGOT FITTING RECEPTACLE ON LH PYLON. REPLACED SPIGOT FITTING RECEPTACLE ON LH PYLON AS PER A319 SRM 54-51-12-300-001. TOOK MEASURE INITIAL ON CORROSION SPIGOT FITTING RECEPTACLE WAS: P1: L:3.058 INCH, P2: L: 1.602 INCH. SEE INDIVIDUAL SIGN OFF 68/400. RII INSPECTION COMPLETE. (LP: 1621285, AIRCRAFT WAS GROUNDED)
LEVEL 2 CORROSION, CORROSION SPIGOT FITTING RECEPTACLE ON RH PYLON. REPLACED SPIGOT FITTING RECEPTACLE ON RH PYLON AS PER A319 SRM 54-51-12-300-001. TOOK MEASURE INITIAL CORROSION SPIGOT FITTINGWAS: P1: L:2.418 INCH, P2: L: 2.872 INCH, SEE INDIVIDUAL SIGN OFF ON ORNRC 52/400. RII INSPECTION COMPLETE. (LP: 1621291, AIRCRAFT WAS GROUNDED)
LEVEL 2 CORROSION, CORROSION SEAT TRACK -Y1292 LOC. FR 64 TO FR 66 AT AFT GALLEY AREA (SSI:534147). REPLACED SEAT TRACK -Y1292 AND FASTENERS LOC. BETWEEN FR64 TO FR66 AT AFT GALLEY AREA AS PER A319 SRM 51-42-11 AS PER A319 SRM51-72-11 AND DWG 10N01048 ISSUE:A RELEASE DATE: 08-SEP-14 TOOK MEASURE ARE L: 2.352 INCH W: 0.364 INCH D=0.037INCH. SEE INDIVIDUAL SIGN OFF ORNRC 36/260 RII INSPECTION COMPLETE. (LP: 1614944) AIRCRAFT WAS GROUNDED
LEVEL 2 CORROSION, SHEAR PLATE STR 23 R LOC. FR 69 TO FR 70 AT AFT GALLEY AREA. APPLIED PROTECTIVE TREATMENT IN NEW HOLES ON SHEAR PLATE IAW SRM 51-21-11,.AND REPLACED SHEAR PLATE LOCATED BTW FR69 TO FR70 AT LEVEL STR23R AT AFT GALLEY AREA IAW SRM 51-42 -11, SRM 51-72-11 AND DWG: D53474180, RELEASE DATE:09/SEP/ 24 ISSUE: AA. MEASURE OF CORROSION AREA L: 2.984 IN W: 1.493 IN. (LP: 1611069) AIRCRAFT WAS GROUNDED
LEVEL 2 CORROSION FR 68 FLOOR SUPPORT -Y765 AT AFT GALLEY AREA. REPLACED THE FLOOR SUPPORT -Y765 LOC. FR 66 TO FR 70 IAW SRM 51-42-11, SRM 51-72-11, DWG D53472780 ISSUE: K AND DWG D53478309 ISSUE E. MEASURE OF THE CORROSION ARE L: 1.298 IN W:1.061 IN D: 0.040 IN. (LP: 1609529) AIRCRAFT WAS GROUNDED.
LEVEL 2 CORROSION, CORROSION CENTER FITTING FR 66 TO FR 68 RH SIDE AT AFT GALLEY AREA ( SSI:534147). REPLACED CENTER FITTING LOCATED FR 66 TO FR 68 RH SIDE AT AFT GALLEY AREA. INITIAL MEASURE OF CORROSION WAS: L:0.4930 IN W: 0.2075 IN D:0.040 IN AS PER A319 SRM 51-42-11 A319 SRM 51-72-11 AND DWG: D53480505 ISSUE: FA RELEASE DATE: 23-MAY-24. SEE INDIVIDUAL SIGN OFF ORNRC 42/260 RII INSPECTION COMPLETE. (LP: 1610737) AIRCRAFT WAS GROUNDED
LEVEL 2 CORROSION, CORROSION SEAT TRACK -Y765 LOC. FR 12 TO FR 24 AT FWD GALLEY AREA (SSI : 531189). REPLACED SEAT TRACK -Y765 LOC. FR 12 TO FR 24 AT FWD GALLEY AREA AS PER A319 SRM 51-72-11 A319 SRM 51-42-11 DWG D53112812 ISSUE: E00 RELEASE DATE: 22-MAR-06 DWG D53110984 ISSUE: C00 RELEASE DATE: 25-JUN-05 DWG D53110920 ISSUE: E00 RELEASE DATE: 28-APR-21 .SEE INDIVIDUAL SIGN OFF ORNRC 32/220 RII INSPECTION COMPLETE. (LP: 1610477) AIRCRAFT WAS GROUNDED
LEVEL 2 CORRIOSION SEAT TRACK -Y765 LOC. FR 64 TO FR 66 AT AFT GALLEY AREA. REPLACED THE SEAT TRACK IAW SRM 51-42-11, SRM 51-72-11, AND DWG NAT10N01048 ISSUE E. MEASURE OF THE CORROSION ARE L: 0.923 IN W: 0.354 IN. (LP: 1609533) AIRCRAFT WAS GROUNDED.
LEVEL 2 CORROSION ON SEAT TRACK -Y1292 LOC BTW FR 12 TO FR 24 AT FWD GALLEY AREA. REPLACED THE SEAT TRACK IAW SRM 51-42-11, SRM 51-72-11, DWG D531128126 ISSUE E00 AND DWG D53110920 ISSUE E00, MEASURES OF THE CORROSION ARE: L= 0.901INCH, W= 0.385 INCH, D= 0.072 INCH. (LP: 1609524) AIRCRAFT WAS GROUNDED.
LEVEL 3 CORROSION, EVIDENCE OF REWORK FLOOR SUPPORT +Y254 LOC. FR 16 TO FR 20 AT FWD GALLEY AREA. REPLACED THE FLOOR SUPPORT Y254 AND FASTENERS LOCATED BTW FR12 TO FR24 AT FWD GALLEY AREA IAW SRM 51-42-11 AND DWG D53112816, ISSUE : G00, DWG D53110984 ISSUE: C00, AND DWG D53110920, ISSUE: E00. (LP: 1609168) AIRCRAFT WAS GROUNDED.
LEVEL 2 CORROSION, ON WEB LOCATED AT LEVEL S23R BTW FR 69 TO FR 70 AFT GALLEY AREA. INSTALLED WEB, BRACKET (1 EA) AND FASTENERS LOCATED AT LEVEL STR23RH BTW FR69 TO FR70 AFT GALLEY AREA AS PER A319 SRM 51-42- 11,DWG: D53474180 ISSUE: E. (LP: 1609200) AIRCRAFT WAS GROUNDED.
ELONGATED HOLES ON COVER SHEET LOCATED FROM FR55A TO FR59 IN AFT CARGO COMPARTMENT. REPLACED COVER SHEET LOCATED FROM FR55A TO FR59 IN AFT CARGO COMPARTMENT IAW SRM 51-42-11, SRM 51-72-11 AND DWG E53476320, ISSUE: BD. MEASURE OF ELONGATED HOLE IS : D = 0.300 INCH (LP: 1607808) AIRCRAFT WAS GROUNDED.
LEVEL 2 CORROSION, ON WEB LOCATED AT LEVEL S23R BTW FR 69 TO FR 70 AFT GALLEY AREA. REPLACED WEB AND FASTENERS LOCATED AT LEVEL S23R BTW FR 69 TO FR 70 AFT GALLEY AREA IAW SRM 51-42-11, DWG D53474180, ISSUE: E. (LP: 1609209) AIRCRAFT WAS GROUNDED.
LEVEL 2 CORROSION FLOOR SUPPORT -Y1292-1162.5 LOC. FR 66 TO FR 68 AT AFT GALLEY AREA. REPLACED FLOOR SUPPORT -Y1292, -Y1162.5 AND LOCATED BETWEEN FR66 TO FR68 AT AFT GALLEY AREA IAW SRM 51-42-11 AND SRM 51-72-11 AND DWG D53472816, ISSUE F, AND DWG D53472780 ISSUE K. TOOK MEASURES OF CORROSION ARE: L= 0.229 INCH, W= 0.217 INCH, D= 0.028 INCH. (LP: 1605825) AIRCRAFT WAS GROUNDED
LEVEL 2 CORROSION, FLOOR SUPPORT -Y1162.5 FROM FR68 TO FR69 AT AFT GALLEY AREA. REPLACED FLOOR SUPPORT -Y1162.5 LOCATED BETWEEN FR68 TO FR69 AT AFT GALLEY AREA IAW SRM 51-42-11 AND A319 SRM 51-72-11 AND DWG D53472780.
DONT PASS OPERATIONAL TEST DAMPER PASSENGER CREW DOOR 832 AT AFT GALLEY AREA. REMOVED DOOR DAMPER OF PASSENGER CREW DOOR 832 ON UNSERVICEABLE CONDITION IAW FAM AMM 52-13-14-000 -001-B EXCEPT STEP 3A ITEM (4) AND 3E. JOB IN PROGRESS. (LP: 1604234) AIRCRAFT WAS GROUNDED
DONT PASS OPERATIONAL TEST DOOR DAMPER ON PASSENGER DOOR 841 AT FWD GA LLEY AREA AT AFT GALLEY AREA. REMOVED DOOR DAMPER OF PASSENGER CREW DOOR 841 ON UNSERVICEABLE CONDITION IAW FAM AMM 52-11-14- 000-001-B. EXCEPT 3.A.(4) AND 3.E. AIRCRAFT WAS GROUNDED
CORROSION FLOOR SUPPORT +Y1162.5 LOC. FR 68 TO FR 69 AT AFT GALLEY AREA (SSI:534147). REPLACED FLOOR SUPPORT Y1162.5 LOC.FR68 TO FR69 AT AFT GALLEY AREA AS PER SRM 51-72-11, A319 SRM 51-42-11 AND DWG D53472780ISSUE: K RELEASE DATE:26-APR-18, DWG: D53474180 ISSUE: AA RELEASE DATE: 09-SEP-24,DWG: D53474250 ISSUE: S RELEASE DATE: 07-SEP-01. MEASURES OF CORROSION WERE L: 0.105 INCH W: 0.046 INCH D: 0.052 INCH. AIRCRAFT WAS GROUNDED
LANDING GEAR DOORS NOT CLOSED, RT DOOR CLOSED, PROXIMITY SENSOR (26GA)TGT POS, LGCIU 1, RT DOOR CLOSED, PROXIMITY SENSOR (28GA) TGT POS, LGCIU 2. FOLLOW TSM TASK 32-31-00-810-861-A. (LP: 1470853)
EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE / LOCATIONS:28D. SEAT BUSSEL THAT HOLDS LIGHT NEEDS TO BE REPAIRED & REPLACED. FWD (28D) EMERGENCY FLR LIGHT TO MEL 33-50-03A. MCC CONTACTED. CREW PLACARD INSTALLED. R & R DAMAGED HOUSING REF A319 AMM 25-21 OK FOR SERVICE MEL AND PLACARD RMVD. (LP: 1400123)
CA 02 MASK MIC IS STUCK ON. RESET UNSUCCESSFUL. COULD NOT DUPLICATE FAULT ON GROUND. CA 02 MASK OPS NML. REF A319 AMM 35-12. (7727314).
OBSERVER'S FIXED SEAT OXYGEN BOX AND MASK LEAKING. R & R OBSERVER STOWAGE BOX AND OXYGEN MASK IAW AMM 35-12. (8223896).
CREW OXYGEN LEAKING AT A RATE OF 41 PSI SINCE LAST SERVICE. R & R THE OBSERVER STOWAGE BOX AND OXYGEN MASK IAW AMM 35-12. (1286068).
FOUND DENT BETWEEN FR10 AND FR11, AND APPR. 12" BELOW STR23 ON THE LEFT. CONFIRMED SURFACE PROTECTION ACCEPTABLE. EVALUATED PER A319 SRM 53-11-11-283-012. (7191121).
SHIP 3169 CATTERING HAD GALLEY CART ROLL INTO SIDE OF LH AFT FUSELAGE BEHIND 2L DOOR. CORRECTIVE ACTION: COMPLIED WITH ER/A 628804-14. (7223438).
DENT AT THE LT FUSELAGE SKIN PANEL AFT OF FR70 AND BETWEEN STGR 16LH AND 17LH. COMPLIED WITH ER/A 628804-14. (1164780).
SHIP 3169 - MISC - DECLARED EMERGENCY DUE TO LOSS OF YELLOW HYDRAULIC SYSTEM FLUID. CORRECTIVE ACTION: REPLACED LEAKING YELLOW HP MANIFOLD PRESSURE SWITCH AND ASSOCIATED SYSTEM FILTERS. (LP 7764502)
SHIP 3169 CRACK ACCESS PANEL 322AL LEADING EDGE ON VERTICAL STABILIZER. CORRECTIVE ACTION: COMPLIED WITH ER/A 627102-14. (1055140).
SHIP 3169 CRACK ACCESS PANEL 322BL LEADING EDGE ON VERTICAL STABILIZER. CORERCTIVE ACTION: COMPLIED WITH ER/A 627100-14. (1055104).
SHIP 3169 CRACK INDICATION ON FRAME 16 LH SIDE IN OPEN FASTENER HOLE H3, AT CROSS BEAM SPLICING AREA. CORRECTIVE ACTION: COMPLIED WITH ER/A 627149-14AD. (1052345).
SHIP 3169 CRACK INDICATION ON FRAME 16 LH SIDE IN OPEN FASTENER HOLE H4, AT CROSS BEAM SPLICING AREA. CORRECTIVE ACTION: COMPLIED WITH ER/A 627149-14AD. (1052350).
SHIP 3169 CRACK INDICATION ON FRAME 16 LH SIDE IN OPEN FASTENER HOLE H2, AT CROSS BEAM SPLICING AREA. CORRECTIVE ACTION: COMPLIED WITH ER/A 627149-14AD. (1052337).
SHIP 3169 FOUND CRACKS AT HOLES #2 #3 AND #4 OF CROSS BEAM JUNCTION AREA, FR16LH. CORRECTIVE ACTION: COMPLIED WITH ER/A 627149-14AD. (1051478).
SHIP 3169, WEAR BONDED BUSHINGS ON UPPER AND LOWER CONNECTION LINK AND SUPPORT ARM OF PASSENGER CREW DOOR 831. REPLACED BUSHES ON UPPER AND LOWER CONNECTION LINK AND SUPPORT ARM OF PASSENGER CREW DOOR 831 AS PER A320 FAM AMM 52-11-21-400- 001-A AS PER A320 FAM AMM 52-11-21-000-001-A AND AS PER A320 FAM AMM-52-10-00-915-001-A.
SHIP 3169 DONT PASS OPERATIONAL TEST EMERGENCY DOOR DAMPER ON PASSENGER CREW DOO R 841. CORRECTIVE ACTION: REPLACED EMERGENCY DOOR DAMPER ON PASSENGER CREW DOOR 841 AS PER A320 FAM AMM-52-11-14-000-001-B AND AS PER A320 FAM AMMAMM-52- 11-14-400-001-B. (1041999)
SHIP 3169 CORROSION ON PLAIN BUSHINGS ON RUDDER HINGE BRACKET SIDE BR7. CORRECTIVE ACTION: REPLACED BUSHINGS OF HINGE #7 ON RUDDER AS PER A319 SRM 51-72-12- 911-002. (1036402).
SHIP 3169 NEED TO COMPLY WITH ERA 622523-14. CORRECTIVE ACTION: COMPLIED WITH ERA 622523-14. (0672127)
SHIP 3169 CAPT SLIDING WINDOW DELAMINATING. CORRECTIVE ACTION: REPLACED PER A319 AMM 56-12. (0523700)
SHIP 3169 DENT ON RT WING INBOARD FLAP. CORRECTIVE ACTION: REPAIRED PER ER/A 615948-14. (5040095)
SHIP 3169 EXISTING REPAIR ON FASTENERS, HOLES NO. C, NO. D LOC. ON FRAME 16 LH SIDE JOG GLE AREA. CORRECTIVE ACTION: COMPLIED WITH ER/A 588166-14 AD REV.A (2877647)
SHIP 3169 OUT OF ADJUSTMENT PASSENGER CREW DOOR 842 POINT H ON UP AND DOWN POSI TION. CORRECTIVE ACTION: PERFORMED ADJUSTMENT ON POINT H IN UP AND DOWN POSITION AS PER A320 FAM AMM 52-13-21-400-001-A. (2876645)
SHIP 3169 EXISTING REPAIR ON FASTENERS HOLES 7, 8, A AND B LOC. ON FRAME 16 RH SIDE JOGGLE AREA. DOCUMENTED ON ER/A 588168-14 AD REV. CORRECTIVE ACTION: COMPLIED WITH ER/A 588168-14 AD REV.A. (2877585)
SHIP 3169 FUSELAGE / FRAME/FORMERS / FR16RH AT DOOR STOP NO 7 LEVEL DOUBLE JOGGLE / HOLES 7 & B / CRACKS. CORRECTIVE ACTION: INSPECTION PER ER/A 588168-14. (2875666)
SHIP 3169 BROKEN FLOOR BEAM -Y1292 BOLT (1 EA) LOC. FR46 IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED BOLT LOC. ON FLOOR BEAM -Y1292 FR46 IN PASSENGER CABIN AS PER A319 SRM 51-42-11. (2874554)
SHIP 3169 FUSELAGE / FRAME/FORMERS / FR16LH AT DOOR STOP NO 7 LEVEL DOUBLE JOGGLE / HOLE C / CRACK. CORRECTIVE ACTION: REPAIRED PER 588166-14. (2873171)
STRONG SMELL OF DE ICE FLUID. C/W ODI PREVENTION AMDS CARD 0550-2002.
OIL SMELL IN CABIN. REMOVED AND REPLACED BOTH RECIRCULATION FILTERS IAW AMM 21- 21-41.
SHIP 3169 - DOOR 2RT DOOR ASSIST BOTTLE LOW. CORRECTIVE ACTION: SERVICED DOOR 2RT DOOR ASSIST BOTTLE PER A319 AMM 52-10-00. (7598916)
SHIP 3169 - ON SVC CHK FOUND 2R POWER ASSIST BOTTLE LOW. CORRECTIVE ACTION: SVC ASSIST BOTTLE PER ALT PROC A321 AMM. (7653831)
R2 DOOR EMERGENCY OPERATING CYLINDER ACCUMULATOR PRESSURE BELOW LIMITS. CORRECTIVE ACTION: SERVICED R2 DOOR EMERGENCY OPERATING CYLINDER PER A319 AMM 52-10. VERIFY SAFETY PIN IN REMOVED AND DAMPER IS ARMED.
DIV-TO BOI FOR ENGINE 1 REVERSER UNLOCKED ECAM MESSAGE. CREW SHUT THE ENGINE DOWN. NO BUFFETING REPORTED. CORRECTIVE ACTION: LOCKED OUT REVERSER AND DEFERRED, PER MEL (12/10 SEA). PERFORMED T/R TEST MULTIPLE TIMES, NO FAULTS. REMOVED AND REPLACED BLOCKER DOOR LATCH, CHECKS OK.
ON POST FLIGHT WALK AROUND IN KGRR, DURING FUELING MISSING CAP. CORRECTIVE ACTION: REPLACED FUEL CAP, OK FOR SERVICE.
CORROSION FLOOR BEAM -Y1292 LOCATED BETWEEN FR 12 TO FR 24 FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED NEW FLOOR BEAM -Y1292 LOCATED BETWEEN FR 12 TO FR 24 FWD GALLEY AREA BRACKETS (6 EA) SPLICE (1 EA) AND FASTENERS, AS PER SRM A319 51-42-11 AND 51-72-11 AND DWG 53112812005 RELEASE DATE 08-JAN-97 ISSUE E00.
CRACK INDICATION ON FRAME 16 LT ON UPPER INBOARD HOLE COMMON TO DOOR STOP FITTING 7. CRACK ON INTERCOSTAL FITTING AT FWD GALLEY AREA. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR ON FRAME 16 LT ON UPPER DOOR STOP FITTING 7, AS PER PRI 588492-14 REV 0 AND ERA 588492-14 AD REV ORIGINAL.
CORROSION FLOOR BEAM -Y765 LOCATED BETWEEN FR 12 TO FR 24 FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM -Y765 LOCATED FR 12 TO FR 24 IN FWD GALLEY AREA, AS PER A319 SRM 51-72-11 AND A319 SRM 51-42-11.
CORROSION FLOOR BEAM +Y1292 AT LEVEL OF FR 20 AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM +Y1292 BETWEEN FR 12 TO FR 24 FWD GALLEY AREA, AS PER A319 SRM 51-72-11 AND DRAWING D53112813 ISSUE G00.
CORROSION RAIL DUMMY Y503.2 AT LEVEL OF FR 16 AT FWD GALLEY AREA. REPLACED RAIL DUMMY Y503.2 AT LEVEL OF FR 16 AT FWD GALLEY AREA 1 EA, AS PER A319 SRM 51-42-11 AND DRAWING D53110984 RELEASE DATE 25-JUN-05; ISSUE C00 AND SRM 51-72-11.
CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOCATED BETWEEN FR 3 TO FR 4 AND 5 INCH ABOVE OF LT LOWER STRINGER LOWER FUSELAGE. CORRECTIVE ACTION: PERFORMED REPAIR LOCATED EXTERNAL SKIN BETWEEN FR 3 TO FR 4 AND 5 INCH ABOVE OF LT LOWER STRINGER, AS PER PRI 588091-14 REV 0 AND ERA 588091-14 REV ORIGINAL.
CORROSION FLOOR STRUCTURE BEAM LOCATED BETWEEN FR 68 TO FR 69 AND - Y1162 IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED FLOOR BEAM AND FASTENERS LOCATED BETWEEN FR 68 TO FR 69 AND -Y1162 IN PASSENGER CABIN, AS PER A319 SRM 51-42-11 AND DWG D53472780 ISSUE K.
CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR TRAILING EDGE UPPER SURFACE OF SLAT 2 ON RT WING. CORRECTIVE ACTION: PERFORMED SECTION I AS PERMANENT REPAIR ON TRAILING EDGE UPPER SURFACE OF SLAT NR 2 ON RT WING, AS PER ER/A 588520-14 REV. ORIGINAL AND PRI NR 588520-14 REV 0.
CORROSION FLOOR BEAM -Y765 BETWEEN FR 66 TO FR 70 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM -Y765 BETWEEN FR 66 TO FR 70 AT AFT GALLEY AREA, AS PER A319 SRM 51-72-11.
CORROSION FLOOR BEAM +Y1227 BETEENW FR 66 TO FR 68 AT AFT GALLEY AREA (1 EA). CORRECTIVE ACTION: REPLACED FLOOR BEAM LOCATED FR 66 TO FR 68 FASTENERS AND SPLICES (4 EA), AS PER SRM A319 51-42-11 AND 51-72-11 AND DWG D53472780 RELEASE DATE 26-APR-18 ISSUE K AND DWG D53472816 RELEASE DATE 18DEC06, ISSUE F. APPLIED PROTECTIVE TREATMENT AND PAINT, AS PER A319 SRM 51-21-11 AND 51-23-11.
CRACK FLOOR STRUCTURE WEB LOCATED BETWEEN FR 68 TO FR 69 LEVEL STR 23L IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED NEW STRUCTURE WEB LOCATED BETWEEN FR 68 TO FR 69 LEVEL STR 23L IN PASSENGER CABIN, AS PER A319 SRM 51-72-11.
CRACK INDICATION ON FRAME 20 LT ON UPPER INBOARD HOLE COMMON TO DOOR STOP FITTING 7. CRACK ON FRAME WEB LAYER AT FWD GALLEY AREA. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTION ON FRAME 20 LT ON UPPER INBOARD HOLE COMMON TO DOOR STOP FITTING 7, AS PER PRI 588192-14 REV 0, REV 1, REV 2 AND ERA 588192-14AD REV ORIGINAL.
CRACK SUPPORT BRACKET COMBUSTION SECTION LOCATED 5 O'CLOCK POSITION ENGINE 1. CORRECTIVE ACTION: REPAIRED SUPPORT BRACKET COMBUSTION SECTION LOCATED 5 O'CLOCK POSITION ENGINE 1, AS PER ERA 564620-14MA REV ORIGINAL SECTION 1.
CRACK INDICATION ON FRAME 4 WINDSHIELD SIDE POST RT SIDE LOWER ATTACHMENT. CORRECTIVE ACTION: PERFORMED REPAIR IN CONJUCTION WITH CARD 5311-01230-01B.
CRACK INDICATION ON FRAME 16 RT SIDE AT OPEN FASTENER HOLE 7, CRACK DIRECTION IS 10 O'CLOCK, AT FWD GALLEY AREA . CORRECTIVE ACTION: PERFORMED REPAIR ON FR 16 RT SIDE AT PASSENGER 7, AS PER PRI 588168-14AD REV 0, 1 AND ERA 588168-14 REV ORIGINAL.
CRACK INDICATION ON FRAME 16 RT SIDE AT OPEN FASTENER HOLE B, CRACK DIRECTION IS 3 O`CLOCK, AT FWD GALLEY AREA. CORRECTIVE ACTION: PERFORMED REPAIR ON FR 16 RT SIDE AT FASTENER HOLE B, AS PER PRI 588168-14AD REV 0, 1 AND ERA 588168-14 REV ORIGINAL.
CRACK INDICATION ON FRAME 16 LT SIDE AT OPEN FASTENER HOLE C, CRACK DIRECTION IS 2 O`CLOCK, AT FWD GALLEY AREA. CORRECTIVE ACTION: PERFORMED REPAIR ON FRAME 16 LT SIDE AT OPEN FASTENER HOLE C, AS PER PRI 588166-14 REV 0 AND REV 1 AND ERA 588166-14 REV ORIGINAL.
CRACK INDICATION ON FRAME 36 AT HOLE A LT SIDE. REPAIR IN ACCORDANCE WITH WORK CARD 5311-01171-04A PRIOR TO FURTHER FLIGHT. CORRECTIVE ACTION: PERFORMED REPAIR IN CONJUCTION WITH WORK CARD 5311-01171-04A.
SHIP 3169 FUSELAGE / FRAME/FORMERS / FR16RH AT DOOR STOP NO 7 LEVEL / DOUBLE JOGGLE / HOLES 7 & B / CRACKS. CORRECTIVE ACTION: REPAIRED PER ER/A 588168-14AD. (1646808)
CRACK INDICATION ON FRAME 4 WINDSHIELD SIDE POST LT SIDE LOWER ATTACHMENT VERTICAL STIFFENER. CORRECTIVE ACTION: PERFORMED REPAIR IN CONJUCTION WITH CARD 5311-01230-01A.
CRACK INDICATION ON FRAME 4 WINDOW LT SIDE POST LOWER ATTACHMENT INTERNAL SIDE IN COCKPIT. CORRECTIVE ACTION: PERFORMED REPAIR IN CONJUCTION WITH CARD 5311-01230-01A.
CRACK INDICATION ON FRAME 4 WINDOW RT SIDE POST LOWER ATTACHMENT INTERNAL SIDE IN COCKPIT. CORRECTIVE ACTION: PERFORMED REPAIR IN CONJUCTION WITH CARD 5311-01230-01B.
CORROSION WEB FRAME 16 RT SIDE AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED WEB LOCATED BETWEEN FR 12 TO FR 16 RT SIDE AT LEVEL STR 23R AT FWD GALLEY AREA, AS PER A319 SRM 51-72-11 AND 51-42-11 AND D53114332, RELEASE DATE:12-DEC-07, ISSUE B00.
CORROSION WEB FRAME 20 RT SIDE AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED WEB LOCATED BETWEEN FR 20 TO FR 24 RT SIDE AT LEVEL STR 23R ON FWD GALLEY AREA, AS PER A319 SRM 51-72-11 AND 51-42-11 AND DRAWING D53112783, RELEASE DATE:28-MAY-98, ISSUE F00.
CRACK INDICATION ON FRAME 36 AT HOLE B RT SIDE. CORRECTIVE ACTION: PERFORMED REPAIR IN CONJUCTION WITH WORK CARD 5311-01171-0413.
SHIP 3169 FUSELAGE / FRAME/FORMERS / FR16LH AT DOOR STOP NO 7 LEVEL / DOUBLE JOGGLE / HOLE C / CRACK. CORRECTIVE ACTION: REPAIRED PER ER/A 588166-14A. (1646639)
SHIP 3169 FUSELAGE / FRAME/FORMERS / FR16RH AT DOOR STOP NO 7 LEVEL / DOUBLE JOGGLE / HOLES 7 & B / CRACKS. CORRECTIVE ACTION: REPAIRED PER ER/A 588168-14. (1646813)
CORROSION LOWER SILL LOCATED FR 20 AT LEVEL STR 23R AT FWD GALLEY AREA. CORRECTIVE ACTION: REPAIRED LOWER SILL LOCATED BETWEEN FR 16 TO FR 20 AT LEVEL STRINGER 23R AT FWD GALLEY AREA, AS PER A319 SRM 51-72-11 AND DRAWING D53110339 ISSUE G00.
CORROSION FLAP TRACK FAIRING 632CB GROUNDING PLATE ON RT WING. CORRECTIVE ACTION: REPLACED GROUNDING PLATE ON FLAP TRACK FAIRING 632CB ON RT WING, AS PER PRI 588132-14 REV 0 AND ERA 588132-14 REV ORIGINAL.
OUT OF ADJUSTMENT PASSENGER CREW DOOR 832 RIGGING POINT (H) ON THE REDUCER SHAFT BELLCRANK IN DOWN POSITION. CORRECTIVE ACTION: PERFORMED ADJUSTMENT PASSENGER CREW DOOR 832 RIGGING POINT (H) ON THE REDUCER SHAFT BELLCRANK IN DOWN POSITION GO THRU ROD (310), AS PER A320 FAM AMM 52-13-21-400-001-A STEP 4G ITEM (1) AND (12) THRU (13) THE ADJUSTMENT IS GOOD.
IMPROPERLY PACKED SLIDE RAFT PASSENGER CREW DOOR 841 AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED SLIDE RAFT PASSENGER CREW DOOR 841 AT FWD GALLEY AREA, AS PER AMDS CARD 2561-4002-RF.
RT FWD DOOR OPEN INDICATION JUST AFTER TOUCHDOWN THEN EXTINGUISHED ON TAXI IN. REMOVED DEBRI FROM DOOR AREA CHECKED GOOD.
COVER TO EMER EXIT HANDLE LOOSE AT LEFT WING EXIT / WINDOW. SECURED LT OVERWING EMERGENCY EXIT COVER HATCH IAW AMM 52- 21.
LT SIDE BOX BEAM UPPER INBD FLANGE AT FRAME 43, AFT HOLE ROTOTEST HFEC SHOWS TWO CRACKS, REPAIRED LT SIDE FR 43 SIDE BOX IAW AMDS CARD 5310-01450-02.
RT SIDE BOX BEAM UPR INBD FLANGE AT FRAME 43, AFT HOLE ROTOTEST HFEC SHOWS TWO CRACKS, REPAIRED RT SIDE BOX BEAM IAW AMDS CARD 5310-01450-02 IAW SB A320-53-1251 REV 1
RT SIDE PRESSURE PLATE AT BOX BEAM UPPER INBD FLANGE AT FRAME 43, AFT HOLE ROTOTEST HFEC SHOWS CRACK, REPLACED PRESSURE PLATE, IAW AMDS CARD 5310-01450-02
NUMEROUS EMERGENCY PATH LIGHTS INOPERATIVE. RELAMPED PATH LIGHTS AND RESECURED 1 CONNECTOR PLUG.
AISLE SEAT EMERGENCY LIGHT LOCATION 20C INOPERATIVE, REPAIR WIRE CONNECTOR AT SEAT 20C.
LIGHTNING STRIKE STATIC PORT ON LOWER FUSELAGE FROM FRAMES 23 - 24 BETWEEN STRINGERS 31 - 33L. PERFORMED TEMPORARY REPAIR IAW ERA 531906-14 REV ORIGINAL.
LIGHTNING STRIKE STATIC PORT, CAPTAIN ON LOWER FUSELAGE ON FRAME 23+13" BETWEEN STRINGER 31L TO STRINGER 33L, PERFORMED TEMPORARY REPAIR ON STATIC PORT CAPTAIN ON LOWER FUSELAGE ON FRAME 23 + 13" BETWEEN STRINGER 31L TO STRINGER 33L AND PERFORMED REWORK ON LIGHTNING STRIKE DAMAGE TO 9 HOLES, AREA IAW SRM 51-73-00, PERFORMED DVI ON REWORKED AREA IAW NTM 51-90-00 TO ENSURE NOT ADDITIONAL DAMAGE EXIST AND PERFORMED HFEC INSPECTION ON REWORKED AREA IAW NTM 51-10-08 TO ENSURE NOT CRACK FREE CONDITION IAW ER/A NR 531906-14, REV .1 AND REV ORIGINAL SECTION 1, 9 HOLES AREAS REPAIR.
CORROSION ON WEB AT FWD GALLEY AREA FROM FRAME 12 - 16 - Y 1732. REPLACED THE WEB IAW SRM 51-72-11 AND DWG D53114392.
DELAMINATED TOP LAYER FLOOR PANEL 261DF AT AFT GALLEY AREA, REPLACED FLOOR PANEL 261DF AT AFT GALLEY AREA.
CORROSION ON FLOOR SUPPORT + Y 1232 BETWEEN FRAMES 66+5 - 67+15. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, 51-42-11 AND DWG D53472816.
CORROSION ON SEAT TRACK -Y1292 BETWEEN FRAMES 64 - 66+5. REPLACED THE SEAT TRACK.
CORROSION ON FLOOR SUPPORT Y 1232 BETWEEN FRAMES 66+5 - 67+15. REPLACED THE FLOOR SUPPORT.
CORROSION ON FLOOR SUPPORT +Y1162 AT AFT GALLEY AREA FROM FRAMES 67+15 - 69. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, 51-42-11 AND DWG D53472000.
CORROSION ON SEAT TRACK +Y765 FRAME 40+3. REPLACED THE SEAT TRACK FROM FRAMES 36 - 41 IAW SRM 51-72-11, DWGS D57130147 AND D53370500.
CORROSION ON FLOOR SUPPORT -Y1162 BETWEEN FRAMES 67+15 - 69. REPLACED THE FLOOR SUPPORT.
CORROSION ON SEAT TRACK -Y765 FRAME 38+2. REPLACED THE SEAT TRACK FROM FRAMES 36 - 41 IAW SRM 51-72-11, DWGS D57130147 AND D53372500.
CORROSION ON LOWER SILL AT AFT GALLEY AREA FROM FRAME 66-FRAME 68 AND STRINGER 23L L=0.675", W=0.430", D=0.001". REPLACED LOWER SILL AT AFT GALLEY AREA FROM FRAME 66 TO FRAME 68 AND STR 23L IAW SRM 51-72-11 AND DRW D53480505; MEASURES OF THE DAMAGE L=0.911", W=0.805", D=0.062".
CORROSION ON WEB FRAMES 69 - 70. REPLACED THE WEB IAW SRM 51-72-11 AND DWG D53470100.
CORROSION ON CENTER FITTING FRAMES 66 - 68 STRINGER 23L. REPLACED THE FITTING IAW SRM 51-72-11 AND DWG D53480009.
CORROSION ON LOWER SILL AT AFT GALLEY AREA FROM FRAME 66 TO FRAME 68 AND STRINGER 23R L=1.115", W=0.860", D=0.001", REPLACED LOWER SILL AT AFT GALLEY AREA FROM FRAME 66 TO FRAME 68 AND STRINGER 23R IAW SRM 51-72-11 AND DWG D53480505, D53474250, MEASURES OF CORROSION ARE: P1 L=2.552", W=1.998", D=0.95" P2 L=1.013" W=0.685".D=0.050" P3 L=1.242" W=1.131" D=0.062" P4 L=2.159" W=0.889" D=0.036".
CORROSION ON SEAT TRACK -Y765 FRAME 44+6. REPLACED THE SEAT TRACK FRAMES 41 - 47 IAW SRM 51-72-11 AND DWG D53370500.
CORROSION ON SEAT TRACK +Y765 FRAME 46+8. REPLACED THE SEAT TRACK FRAMES 41 - 47 IAW SRM 51-72-11 AND DWG D53370500.
CORROSION ON SEAT TRACK +1292 FRAME 46+9. REPLACED THE SEAT TRACK FRAMES 41 - 46 IAW SRM 51-72-11 AND DWG D53372500.
CORROSION ON CORNER FITTING, FRAME 68. REPLACED THE FITTING IAW SRM 51-72-11 AND DWG D53480019.
CORROSION ON CORNER FITTING, FRAME 68. REPLACED THE FITTING IAW SRM 51-72-11 AND DWG D53480019.
CROSSBEAM +Y1232 FRAME 67 DAMAGED. REPLACED THE CROSSBEAM IAW SRM 51-72-11 AND DWG D53424250.
CORROSION ON WEB FRAMES 69 - 70 STRINGER 23L . REPLACED THE WEB IAW SRM 51-72-11 AND DWG D53470100.
CORROSION ON WEB FRAME 69 - 70 STRINGER 23L. REPLACED THE WEB IAW SRM 51-72-11 AND DWG D53470100.
CRACK ON FRAME 67 BETWEEN STRINGER 23 - 26R, REPLACED FRAME ANGLE IAW 51-72-11, DWG D53480076, AND D53480019.
CORROSION ON FLOOR PANEL 221FF IN FWD GALLEY. REPLACED THE FLOOR PANEL.
CORROSION ON FLOOR PANEL 261FF. REPLACED THE FLOOR PANEL.
CORROSION ON CORNER FITTING FRAME 66 S23R. REPLACED THE FITTING IAW SRM 51-72-11 AND DWG D5348-0505.
CORROSION ON SEAT TRACK +Y1292 FRAME 37+4. REPLACED THE SEAT TRACK FRAMES 36 - 41IAW SRM 51-72-11 AND DWG D53372500.
CORROSION ON SEAT TRACK -Y1292 FRAME 35+14. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D53374044.
CORROSION ON FLOOR SUPPORT Y1732 BETWEEN FRAMES 65 - 66. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG E53474250.
CORROSION ON SEAT TRACK -Y1292 FRAMES 42+18. REPLACED THE SEAT TRACK FRAMES 42 - 46 IAW SRM 51-72-11, DWG D53370500, AND D53372500.
CORROSION ON CENTER FITTING AT FWD GALLEY AREA FROM FRAMES 16 - 20. REPLACED THE FITTING IAW SRM 51-72-11 AND DWG D5311-2109.
CORROSION ON FLOOR PANEL 222FF AT FWD GALLEY AREA. REPLACED THE FLOOR PANEL.
CORROSION ON CORNER FITTING FRAME 20. REPLACED THE FITTING IAW SRM 51-72-11 AND DWG D53112109.
CRACK ON CROSSBEAM FRAME 68. REPLACED THE CROSSBEAM IAW SRM 51-72-11 AND DWG D5347-0150.
CORROSION ON CENTER FITTING FRAMES 16 - 20 STRINGER 23R. REPLACED THE FITTING IAW SRM 51-72-11 AND DWG D53112109.
CORROSION ON FLOOR PANEL 262FF. REPLACED THE FLOOR PANEL.
CORROSION ON FLOOR PANEL 221LF ALL INSERT AT FWD GALLEY AREA. REPLACED THE FLOOR PANEL.
CORROSION ON FLOOR SUPPORT +Y1292 FRAMES 12 - 24. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, DWG D53112812, AND D53110984.
CORROSION ON FLOOR SUPPORT AT AFT GALLEY AREA - Y 465 BETWEEN FRAMES 64 - 67+10. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472816.
CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 65 - 66. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53470150.
CORROSION ON FLOOR SUPPORT -Y765 BETWEEN FRAMES 66+5 - 70. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.
CORROSION ON FLOOR SUPPORT -Y765 BETWEEN FRAMES 64 - 66+5. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472832.
CORROSION ON FLOOR SUPPORT +Y765 BETWEEN FRAMES 66+5 - 70. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.
CORROSION ON FLOOR SUPPORT -Y1292 FRAMES 12 - 24. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, DWG D53112812, AND D53110920.
CORROSION ON FLOOR SUPPORT +Y512 BETWEEN FRAMES 64 - 67+10. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472816.
CORROSION ON FLOOR SUPPORT +Y765 FRAMES 64 - 66. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472831.
CORROSION ON FLOOR PANEL 221EF INSERT AT FWD GALLEY AREA. REPLACED THE FLOOR PANEL IAW SRM.
CORROSION ON DUMMY RAIL Y503.2 FRAMES 12 - 16. REPLACED THE DUMMY RAIL IAW SRM 51-72-11 AND DWG D53112825.
EMERGENCY LIGHTS IN FWD GALLEY AND ROWS 1, 2, 5, AND 6 INOPERATIVE. REPLACED POWER SUPPLY & BATTERY PACK IAW AMM 33-51. OPS CHECKED GOOD.
RT WING L/E PANEL LANDING BETWEEN SLAT TRACK NR 5 THROUGH NR 6 INBD SIDE WORN. REMOVED DISCREPANT PANEL LANDING. INSTALLED NEW LAND IAW TRM 57-27-13. COMPLIED WITH PERMANENT REPAIR IAW TRM 57-27-13.