N941FR

AIRBUS A319-112 · 2005 · Valid Registration

Registered owner: UMB BANK NA TRUSTEE, UT (owner ≠ operator)

Operators of this aircraft

Who operated this tail, and how firmly we know it.

OperatorRolePeriodBasis
FRONTIER AIRLINES, INC. (F3LA)Operator2015-05-04 – 2015-05-04Operator named in NTSB report
Frontier AirlinesOperator2015-05-04 – 2015-05-04Operator named in NTSB report

Accident & incident history

Inc · 2015-05-04 Operator named in NTSB report
AIRBUS A319 112 None injury Part 121FRONTIER AIRLINES, INC.
Source: NTSB case CEN15IA225

Maintenance disclosures

L · 2021-04-02 Matched by certificate designator
ATA 3350

DISCREPANCY: LP1264105 ITEM 1- EPSU 10WL FAILED EPSU SYS TEST. FOUND 10WL BATTERY EXPIRED, CORRECTIVE ACTION: R&R BATTERY & FAULT CONTINUED, R&R EPSU UNIT FAULT CLEARED, TEST OK AT THIS TIME REF AMM 33-51-38-04- CONF 00.

Source: SDR F3LA2021040200028 · FAA SDRS
J · 2019-12-11 Matched by certificate designator
ATA 7320

DISCREPANCY: LP1229399 ITEM , ENGINE 2 CTL VALVE FAULT OCCURRED ON T/O. ABORTED T/O @ 80 KTS, 137,000LB, TEMP 2 C. CORRECTIVE ACTION: REPLACED ENGINE #2 ECU. OPS TEST GOOD, OK TO CONTINUE. PERFORMED LAND TEST. OPS NORMAL. AIRCRAFT RETAINED CATIIIB STATUS. REF. AMM 73-21-60-000-001-B AND 73-21-60-400-001-B.

Source: SDR F3LA201912120153 · FAA SDRS
O · 2019-09-23 Matched by certificate designator
ATA 5310

L1 DOOR CUTOUT, UPPER FWD CORNER, AFT FASTENER ROW, LWR 1 /4" HOLE, CRACK INDICATION, BOTTOM OF OUTER LAYER, 2:30 OCLOCK ORIENTATION. REPAIRED L1 DOOR FR 16 HOLE# 1 PER AIRBUS RDAS REF: 80686917 /003/2019 REPAIR INSPECTION THRESHOLD =6800FC WITH INTERVALS OF, 4,823FC

Source: SDR F3LA201910090123 · FAA SDRS
F J · 2018-09-10 Matched by certificate designator
ATA 2750

FLIGHT CONTROL FLAPS LOCKED AFTER SELECTING FLAPS 2. ADJUSTED RIGHT FLAP INTERCONNECTING STRUT. RIG AND OPS CHECK GOOD. REFERENCE AMM 27-51-44-820-001A.

Source: SDR F3LA2018091400431 · FAA SDRS
F J · 2018-09-07 Matched by certificate designator
ATA 2750

OPERATIONAL CHECK FLIGHT UNSATISFACTORY. AFTER 3RD TIME OF EXTENDING FLAPS (12000FT 170KTS) ECAM, F/CTL FLAPS LOCK-ALIGNMENT FAULT. SLATS AT GREEN 2, FLAPS AMBER 0. VISUAL INSPECTION SHOWS FLAPS 1. PERFORMED POST FLIGHT WALK AROUND, NO DEFECTS NOTED. FOUND MISSING HARDWARE AT NR 3 FLAP DRIVE ATTACH POINT. HARDWARE WAS REINSTALLED AND FLAP RIG CHECK. AC OK FOR SERVICE. AMM 27-54-62-420-077 / 27-51-00-820-003A.

Source: SDR F3LA2018091000428 · FAA SDRS
N · 2018-09-04 Matched by certificate designator
ATA 2750

F/CTL FLAPS LOCKED - ALIGNMENT FAULT. PERFORMED BITE TEST OF SFCC 1 AND 2 NO FAULTS NOTED. OPS CHECK GOOD AMM 27-51-00-740-002-A.

Source: SDR F3LA2018090600425 · FAA SDRS
F J · 2018-09-03 Matched by certificate designator
ATA 2750

F/CTR FLAPS LOCKED. PERFORMED BITE TEST OF SFCC 1 AND 2 MESSAGE CLEARED. PERFORMED OPS CHECK OF FLAPS. OPS CHECK GOOD AT THIS TIME. AMM 27-51-00-740-002-A AND 27-51-00-710-001.

Source: SDR F3LA2018090600423 · FAA SDRS
O · 2017-10-07 Matched by certificate designator
ATA 5320

CABIN AFT WET AREA, Y765 AT FRAMES 66 - 70 FLOOR SUPPORT CORRODED. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 53-00-14, SRM 51-72-11-911-001, AND 51-44-00.

Source: SDR F3LA2017101100235 · FAA SDRS
O · 2017-10-07 Matched by certificate designator
ATA 5320

CABIN AFT WET AREA, LT SHEAR WEB CRACKED AT FRAMES 68 - 70. REMOVED AND REPLACED THE SHEAR WEB IAW SRM 51-42-11, 51-72-11-911-001, AND 51-44-11.

Source: SDR F3LA2017101700240 · FAA SDRS
O · 2017-10-07 Matched by certificate designator
ATA 5320

CABIN AFT FLOOR SUPPORT Y512 CORRODED AT BOLT HOLES FRAME 66. REMOVED AND REPLACED THE FLOOR SUPPORT FROM FRAMES 64 -66 IAW SRM 51-42-11, AND 51-72-11-911-001.

Source: SDR F3LA2017101000232 · FAA SDRS
O · 2017-10-07 Matched by certificate designator
ATA 5320

CORROSION FOUND ON THE FLOOR SUPPORT, Y 765, FRAMES 65-66. REMOVED AND REPLACED THE FLOOR SUPPORT IAW 51-72-11-911-001, AND 51-44-11.

Source: SDR F3LA2017101000231 · FAA SDRS
O · 2017-10-07 Matched by certificate designator
ATA 5315

CABIN AFT WET AREA FLOORBEAM Y1292 CORRODED AT FRAME 66. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-11, AND 51-72-11-911-001.

Source: SDR F3LA2017101100234 · FAA SDRS
O · 2017-10-05 Matched by certificate designator
ATA 5320

RIGHT FLOOR SUPPORT -Y1292 CORRODED ON THE TOP SURFACE FRAMES 66 - 68. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11 AND 51-72-11-911-001.

Source: SDR F3LA2017101600236 · FAA SDRS
O · 2017-10-05 Matched by certificate designator
ATA 5315

FLOORBEAM -Y765 CORRODED ON TOP SURFACE AT FRAME 68. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-72-11-911-001, 51-42-11, AND 51-44-11.

Source: SDR F3LA2017101000233 · FAA SDRS
O · 2017-10-05 Matched by certificate designator
ATA 5315

RIGHT FLOORBEAM -Y1292 CORRODED ON THE TOP SURFACE AT FRAME 66. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-11, 51-72-11-911-001, AND 51-44-71.

Source: SDR F3LA2017101600238 · FAA SDRS
O · 2017-10-05 Matched by certificate designator
ATA 5315

RIGHT FLOORBEAM -Y1162, FRAME 68. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-11, AND 51-72-11-911-001.

Source: SDR F3LA2017101600239 · FAA SDRS
O · 2017-10-05 Matched by certificate designator
ATA 5320

R2 DOOR SILL CORRODED ON THE TOP SURFACE AT FRAME 68. REMOVED AND REPLACED THE DOOR SILL, FRAMES 66 - 68 IAW SRM 51-42-11, AND 51-72-11-911-001.

Source: SDR F3LA2017101600237 · FAA SDRS
L · 2017-09-25 Matched by certificate designator
ATA 3350

EPSU TEST FAULT 11WL.. REMOVED AND REPLACED EPSU 11WL BATTERY IAW AMM 33-51-38-PB401. OPS CHECKED GOOD.

Source: SDR F3LA2017092500229 · FAA SDRS
L · 2017-06-18 Matched by certificate designator
ATA 3350

EPSU 10WL, 12WL AND 13WL FAILED BATTERY CAPACITY TESTS IAW 33-51-00-710-003-A. REMOVED AND REPLACED EPSU. OPS TESTED GOOD IAW AMM 33-51-38 PB 401.

Source: SDR F3LA2017062000180 · FAA SDRS
O · 2015-05-04 Matched by certificate designator
ATA 5610

RIGHT WINDSHIELD CRACKED AT 34,000 FEET. REPLACED FIRST OFFICERS WINDSHIELD IAW AMM 56-11-11-401.

Source: SDR F3LA2015050701131 · FAA SDRS
L · 2015-03-04 Matched by certificate designator
ATA 3350

EPSU EMER LIGHTS BATTERY 12WL RT FAILED THE CAPACITY CHECK DURING A SCHEDULED A8 CHECK, TASK CARD FFT-335100-03-1. R & R EPSU EMER BATTERY 12WL RT IAW AMM 33-51-38 PB 401. OPERATIONS CHECK IS GOOD.

Source: SDR F3LA2015030401111 · FAA SDRS
L · 2015-03-04 Matched by certificate designator
ATA 3350

EPSU BATTERY 10WL, FWD LT FAILED CAPACITY TEST ON TASK CARD FFT-335100-03-1 ON SCHEDULED A8 CHECK. R & R BATTERY ASSEMBLY IAW AMM 33-51-38-000-002A & AMM 33-51-38-400-002A.

Source: SDR F3LA2015030401109 · FAA SDRS
L · 2015-03-04 Matched by certificate designator
ATA 3350

EPSU EMER LIGHTS, BATTERY 11WL LT FAILED THE CAPACITY CHECK DURING A SCHEDULED A8 CHECK. TASK CARD FFT-335100-03-1, R & R EPSU EMER BATTERY 11WL LT IAW AMM 33-51-38 PB 401. OPERATIONS CHECK IS GOOD.

Source: SDR F3LA2015030401110 · FAA SDRS
L · 2015-03-04 Matched by certificate designator
ATA 3350

EPSU BATTERY 13WL, AFT LT, FAILED CAPACITY TEST ON TASK CARD FFT-335100-03-1 ON SCHEDULED A8 CHECK. R & R BATTERY ASSEMBLY IAW AMM 33-51-38-000-002A & AMM 33-51-38-400-002A.

Source: SDR F3LA2015030401112 · FAA SDRS
K J · 2014-07-22 Matched by certificate designator
ATA 2910

AFTER TAKEOFF GREEN HYD SYS FAILURE LOW RES & LOW HYD PRESS MESSAGES. EMER DECLARED. REPLACED FLEXIBLE HOSE FOR RT GEAR DOOR ACTUATOR, AFT HOSE IAW AMM 32-31-39 PAGE BLOCK 401.

Source: SDR F3LA2014072401049 · FAA SDRS
L · 2014-05-21 Matched by certificate designator
ATA 2565

EMERGENCY LIGHTING SYS FAILED FUNCTIONAL CHECK DURING ROUTINE MX CHECK HEAVY SERVICE. R & R LT FWD EMER ESCAPE SLIDE LAW AMM 25-62-44 PB 401. OPERATIONAL CHECK GOOD.

Source: SDR F3LA2014052301039 · FAA SDRS
O · 2014-05-04 Matched by certificate designator
ATA 5320

AFT CABIN RT LATERAL SHEAR PLATE HAS CORROSION. R & R RT LATERAL SHEAR PLATE IAW 51-42-11 PAR 6, 7 & 13 EO A0-53EO-31434.

Source: SDR F3LA2014051401038 · FAA SDRS
O · 2014-05-04 Matched by certificate designator
ATA 5320

AFT CABIN LT LATERAL SHEAR HAS CORROSION. R & R LT LATERAL SHEAR PLATE IAW 51-42-11 PAR 6, 7 & 13 EO A0-53EO-31434.

Source: SDR F3LA2014051401037 · FAA SDRS
O · 2014-04-30 Matched by certificate designator
ATA 5320

RT SERVICE DOOR HAS CORROSION AFT INBD END AT FRAME 68. REMOVED CORROSION & REPAIRED THRESHOLD IAW SRM 53-41-14 PB 201 FIG 201.

Source: SDR F3LA2014051401035 · FAA SDRS
O · 2014-04-30 Matched by certificate designator
ATA 5315

FLOOR BEAM AT FRAME 67 L2 DOOR HAS CORROSION. CORROSION BEYOND LIMITS, R & R FLOOR BEAM IAW SRM 51-42-11 PAR 5 A-C.

Source: SDR F3LA2014051401036 · FAA SDRS
L · 2012-05-18 Matched by certificate designator
ATA 3350

SEAT ROW 4ABC EMERGENCY EXIT LIGHT INOPERATIVE. R & R BULB EMERGENCY EXIT LIGHT IAW AMM 33-51-18, PB 401.

Source: SDR F3LA2012052300758 · FAA SDRS
B · 2011-07-16 Matched by certificate designator
ATA 2150

DURING APPROACH 8,000 MSL, WHISTLE AND SMOKE COMING FROM LONG A/C VENT. NO ECAM CHECKED AIR COND PAGE LOWER SCREEN AIR WAS 100+ FROM PACK ONE. LANDED AND MECHANIC HAD TURNED PACK 1 ON AND OFF AND SMELLED SMOKE. PERFORMED TROUBLESHOOTING OF PACK 1 OVERHEAT MESSAGE PER TSM 21 -61-00-810-801. CONFIRMED NR 1 PACK TO BE SOURCE OF SMOKE. NR 1 PACK DEFERRED PER MEL 21 -520 LD.

Source: SDR F3LA2011072100661 · FAA SDRS
O · 2011-04-29 Matched by certificate designator
ATA 5320

C-CHECK: NON ROUTINE NR 35292; RT SIDE LATERAL SHEAR PLATE HAS CORROSION AT FASTENER HOLES. R & R SHEAR PLATE WITH NEW CONFIGURATION IAW EO AO-53EO-31 AND SRM 51-42-11, PARA 6B 1-8, PARA 7B 2A-C AND PARA 13D 1-6, SRM 51-21-11 PARA 2C, 3C.

Source: SDR F3LA2011050300638 · FAA SDRS
K J · 2010-08-30 Matched by certificate designator
ATA 2910

AIR TURN BACK, HYD GREEN RESERVOIR LOW LEVEL ECAM IN FLIGHT. 54COMPLETED ECAM, VOL II PROCEDURES AND GRAVITY LANDING GEAR EXTENSION PROCEDURE. PILOT REPORT EMERGENCY DECLARED. R & R LT MLG GEAR DOOR ACTUATOR FLEXIBLE HYD LINE. REF AMM 32-12-00-991-015. PERFORM OPS AND LEAK TEST OF THE GREEN HYD SYS REF AMM 29-11-00-710-001. OPS NORMAL, NO LEAK PLACE THE ACFT TO NORMAL CONFIGURATION REF AMM 32-00-00-860-003.

Source: SDR F3LA2010090100492 · FAA SDRS
O · 2009-11-03 Matched by certificate designator
ATA 5320

REF NON ROUTINE C073471. DURING DEN C3 C-CHECK, INSP NOTED CORROSION ON THE L2 THRESHOLD PANEL 261FF. MX REMOVED AND REPLACED THE PANEL IAW AMM 53-42-12-400-002.

Source: SDR F3LA2009110500224 · FAA SDRS
O · 2009-11-02 Matched by certificate designator
ATA 5320

REF NON ROUTINE C073470. DURING DEN C3 C-CHECK, INSP NOTED CORROSION ON THE R3 THRESHOLD PANEL 262FF. MX REMOVED AND REPLACED THE FLOOR PANEL IAW AMM 53-42-12-400-002.

Source: SDR F3LA2009110500225 · FAA SDRS
O · 2009-10-30 Matched by certificate designator
ATA 5320

REFERENCE NON ROUTINE C073394. DURING DEN C3 C-CHECK, INSPECTION NOTED CORROSION ON THE FLOOR SUPPORT NUT CLIP HOLES LOCATED AT STATION -Y1292 BETWEEN FRAMES 68 AND 69. MX REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-44-11, 51-42-11 AND 51-75-11.

Source: SDR F3LA2009110200223 · FAA SDRS
O · 2009-10-29 Matched by certificate designator
ATA 5320

REFERENCE NON ROUTINE C073186. DURING DEN C3 C-CHECK, INSP NOTED CORROSION ON THE FLOOR SUPPORT NUT CLIP HOLES LOCATED AT STATION Y1292 BETWEEN FRAMES 66 AND 68. MX REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-44-11, 51-42-11 AND 51-72-11.

Source: SDR F3LA2009110200222 · FAA SDRS
O · 2009-10-29 Matched by certificate designator
ATA 5320

REFERENCE NON ROUTINE C073187. DURING DEN C3 C-CHECK, INSP NOTED CORROSION ON THE FLOOR SUPPORT NUTCLIP HOLES LOCATED AT STA -Y1292 BETWEEN FRAMES 66 AND 68. MX REMOVED AND REPLACED THE FLOOR BEAM ASSY IAW SRM 51-44-11 AND 51-42-11.

Source: SDR F3LA2009110200221 · FAA SDRS
O · 2008-07-15 Matched by certificate designator
ATA 5321

DURING C2 C-CHECK, INSPECTION NOTED THE AFT PIT TRANSITION PANEL 161BF WAS PUNCTURED. MAINTENANCE REPAIRED DAMAGE IAW THE REQUIREMENTS OF A319 SRM 53-02-00, PARAGRAPH 8C FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)

Source: SDR F3LA200800498 · FAA SDRS
B · 2008-07-09 Matched by certificate designator
ATA 2120

DURING TAXI THE F/A NOTICED A FAINT ODOR FOR A DURATION LESS THAN FIVE SECONDS. DURING TAKEOFF ROLL THE F/A NOTICE THAT SAME DOOR AGAIN. THE ODOR WAS LOCATED IN THE AFT GALLEY ON THE LT SIDE OF THE ACFT. NO OTHER OCCURANCES WERE NOTED FOR THE DURATION OF THE FLIGHT. MAINT PERFORMED AN AIR QUALITY TEST IAW TSM 21-00-00-810-802. THE AC WAS INSPECTED AND NO SOURCE OF ODOR WAS LOCATED AND THE AC CONTINUED SERVICE. (B)

Source: SDR F3LA200800440 · FAA SDRS
O · 2008-06-20 Matched by certificate designator
ATA 2613

DURING C-CHECK INSP NOTED OPS TEST OF APU AUTO FIRE EXTINGUISHING EXITING CIRCUIT AND THE APU LOW PRESSURE VALVE OPERATION USING EACH INDIVIDUAL MOTOR IN TURN AND TEST APU EMERGENCY SHUTDOWN CIRCUIT FAILS. MAINT REMOVED AND REPLACED RELAY 39WF AND OPS CHECKED GOOD. ALL WORK WAS COMPLETED IAW TSM 26-22-00-810-804 AND AMM 26-22-00-710-002. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Source: SDR F3LA200800381 · FAA SDRS
O · 2008-06-19 Matched by certificate designator
ATA 5755

DURING C-CHECK INSP, NOTED LT WING NR FOUR SPOILER ATTACH BOLT IS ROTATED IN LUG ON SPOILER. MAINT MACHINED .040 OFF ANTI-ROTATION WEB VERIFIED SS MATERIAL FOR REPAIRED PO RT090486 AND BONDED AND THE REINFORCING PLATE TO THE ANTI-ROTATION WEB FOR THE CENTER HINGE IAW EA A9-57R-30397 STEPS 3, 4, 5, AND 6. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Source: SDR F3LA200800375 · FAA SDRS
O · 2008-06-18 Matched by certificate designator
ATA 5321

DURING C-CHECK INSP, NOTED AFT PIT SCREW PULLING THROUGH FLOOR PANEL 151CE NEXT TO FORWARD TIE DOWN BY SILL PLATE. MAINT REPAIRED PANEL 151CE IAW EA A0-53T-10131. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Source: SDR F3LA200800374 · FAA SDRS
O · 2008-06-16 Matched by certificate designator
ATA 5321

DURING C-CHECK INSP, NOTED AFT PIT FLOOR PANEL 151CE HAS SEVERAL PUNCTURES. MAINT REPAIRED PANEL 151CE IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Source: SDR F3LA200800367 · FAA SDRS
O · 2008-06-16 Matched by certificate designator
ATA 5210

DURING C-CHECK INSP, NOTED L1 DOOR HOLD OPEN LATCH BUTTON FAILED PRESS TEST. MAINT ADJUSTED L1 DOOR BUFFER IAW AMM 52-11-00-820-001 STEP 4J. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Source: SDR F3LA200800359 · FAA SDRS
O · 2008-06-16 Matched by certificate designator
ATA 5320

DURING C-CHECK INSP NOTED AFT PIT TRANSITION PANEL 151HE HAS SEVERAL PUNCTURES. MAINT REPAIRED PANEL 151HE IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Source: SDR F3LA200800362 · FAA SDRS
O · 2008-06-16 Matched by certificate designator
ATA 5321

REFERENCE NON ROUTINE C045369. DURING C2 C-CHECK INSPECTION NOTED AFT PIT FLOOR PANEL 151PE HAS SEVERAL PUNCTURES. MAINTENANCE REPAIRED PANEL 151PE IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 53-02-00 PARAGRAPH 8C FUGURE 204. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Source: SDR F3LA200800368 · FAA SDRS
O · 2008-06-16 Matched by certificate designator
ATA 5320

DURING C-CHECK INSP, NOTED AFT PIT TRANSITION PANEL 152UG HAS SEVERAL PUNCTURES. MAINT REPAIRED PANEL 152UG IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Source: SDR F3LA200800366 · FAA SDRS
O · 2008-06-16 Matched by certificate designator
ATA 5321

DURING C2 C-CHECK, INSPECTION NOTED AFT PIT TRANSITION PANEL 151DE HAS SEVERAL PUNCTURES. MAINTENANCE REPAIRED PANEL IN ACCORDANCE WITH A319 SRM 53-02-00, FIGURE 204.

Source: SDR F3LA200800365 · FAA SDRS
O · 2008-06-16 Matched by certificate designator
ATA 5320

DURING C-CHECK INSP NOTED AFT PIT TRANSITION PANEL 151FE HAS SEVERAL PUNCTURES. MAINT REPAIRED PANEL 151FE IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Source: SDR F3LA200800363 · FAA SDRS
L · 2008-06-16 Matched by certificate designator
ATA 5210

DURING C-CHECK INSP, NOTED L2 DOOR HOLD OPEN LATCH BUTTON FAILED PRESS TEST. MAINT ADJUSTED L2 DOOR BUFFER IAW AMM 52-13-00-820-001 STEP 4J. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Source: SDR F3LA200800358 · FAA SDRS
L · 2008-06-16 Matched by certificate designator
ATA 5240

DURING C-CHECK INSP, NOTED R1 DOOR HOLD OPEN LATCH BUTTON FAILED PRESS TEST. MAINT ADJUSTED R1 DOOR BUFFER IAW AMM 52-11-00-820-001 STEP 4J. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Source: SDR F3LA200800361 · FAA SDRS
O · 2008-06-16 Matched by certificate designator
ATA 5240

DURING C-CHECK INSP NOTED R2 DOOR HOLD OPEN LATCH BUTTON FAILED PRESS TEST. MAINT ADJUSTED R2 DOOR BUFFER IAW AMM 52-11-00-820-001 STEP 4J. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Source: SDR F3LA200800360 · FAA SDRS
O · 2008-06-16 Matched by certificate designator
ATA 5320

DURING C-CHECK INSP, NOTED AFT PIT TRANSITION PANEL 151GE HAS SEVERAL PUNCTURES. MAINT REPAIRED PANEL 151GE IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Source: SDR F3LA200800364 · FAA SDRS
B · 2006-11-05 Matched by certificate designator
ATA 2120

DURING CRUISE, PAX/FLT ATTN REPORTED A BURNING RUBBER ODOR AT ROWS 2, 3 AND 4. FLIGHT CREW DECLARED AN EMERGENCY AND DIVERTED TO SLC. AIRCRAFT LANDED WITHOUT INCIDENT, TAXIED TO THE GATE AND THE PAX WERE DEPLANED. THE AIRCRAFT WAS INSPECTED IAW AMM 24-00-00-810-823, 26-15-00-810-804 AND 31-50-00-710-001. NO DEFECTS OR ODOR NOTED. PLACED LIVE TV ON MEL 44-20-01AA AS PRECAUTIONARY. AIRCRAFT RELEASED FOR SERVICE. UPON ARRIVAL, MAINTENANCE PERFORMED ELECTRICAL ODOR SYSTEM INTEGRITY CHECK IAW LTV AMM 44-25-00, PAGE 5036, 5037, AND 5038. OPS CHECK GOOD. REMOVED MEL PLACARD.

Source: SDR F3LA200600149 · FAA SDRS