N838UA

Service difficulty reports · 93

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE n_number = 'N838UA' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR CALA2026061717147Fuel Cap · missingFUEL CAP MISSING REQUIRES PDA UNABLE TO LOCATE FUEL CAP AT STATION PLACED ON CDL LP: 9255512 - FUEL CAP MISSING THE CAPTAIN VERIFIED NO LEAKAGE FROM THE COUPLING. INOP STICKER IS INSTALLED ADJACENT TO THE REGISTRATION NUMBER ON THE FORWARD INSTRUMENT PANEL. REJun 14, 2026 · N838UA · Airbus A319131 · Fuel StorageSDR CALA2025102710616Isolation Valve · faultedAIR X BLEED FAULT ON CLIMB OUT PFR SHOWS 36-12 AIR X BLEED FAULT W/ CORRELATED MSG'S 36-11-34 BMC 1 OR SOLENOID, 36-12-00 X FEED VALVE 6HV AND 36-12-00 X FEED VALVE 6HV OR CKT. ACP BMC 1 & 2 BITE CHKS GOOD ON THE GRND ALSO OPERATED X BLEED SWITCH AND ALL ECAMOct 24, 2025 · N838UA · Airbus A319131 · Pneumatic Distribution SystemSDR CALA2025101610166Unknown · odorMUSTY SMELL IN COCKPIT UPON ARRIVAL AT A/C UPON ARRIVAL TO AIRCRAFT THE ODOR WAS VERY FAINT AND ALMOST GONE. FOLLOWED FIM TASK 05-50-00-810-831-A. AIRPLANE HAS HISTORY OF HYDRAULIC LEAK AND SUSPECT RESIDUAL HYDRAULIC FLUID GOT INTO APU INLET AND HAD MOMENTARY Oct 15, 2025 · N838UA · Airbus A319131 · Air Distribution SystemSDR CALA2025082007949Indicator · no discrepancyAFT CARGO DOOR GREEN LATCH INDICATORS ARE NOT VISIBLE. INSPECTED LATCHES FOR ALL GREEN INDICATIONS, ALL ARE GREEN OK TO CONTINUE. AAug 16, 2025 · N838UA · Airbus A319131 · Cargo/Baggage DoorsSDR CALA2025081107527Exciter · faultedHUNG START ON NUMBER 1 ENGINE AFTER STARTER CUT OUT. STRONG FUEL ODOR IN FLTDECK AFTER CRANK CLASS 3 FUEL DEPULSE ACTIVATED 1. LEADS TO TSM 80-00-00-810-819-A. ENG START INITIAL TO IDLE SPEED TOOK 2 PLUS MINUTES ON 2 STARTS. ODOR OF FUEL SMELL IN FLIGHT DECK UAug 11, 2025 · N838UA · Airbus A319131 · ExciterSDR CALA2025080807484Door · leakingLOUD NOISE FROM RIGHT SIDE EMERGENCY EXIT, NOISE ALREADY ON DIP. INSPECTED EXISTING SPEED TAPE, FOUND MULTIPLE AREAS PEELING. REMOVED AND REAPPLIED DAMAGED SPEED TAPE.Aug 7, 2025 · N838UA · Airbus A319131 · Emergency ExitsSDR CALA2025061305534Cover · detachedSLIDE ARMED INDICATOR COVER FOUND ON FLOOR IN FRONT OF 1L. ACCOMPLISHED INTERIM REPAIR PER PART 1, INSPECT EACH FLIGHT, AND ACCOMPLISH PERMANENT REPAIR WITHIN 3 DAYS.Jun 10, 2025 · N838UA · Airbus A319131 · Door Warning SystemSDR CALA2025052304923Idg · faultedACFT RETURN TO FIELD, CREW STATED ALL FAULTS STARTED TO OCCUR AT WHEELS OFF GROUND. FIRST FAULTS ON PFR INDICATE ELEC AC BUS 2 FAULT, ELEC DC BUS 2 FAULT, ELEC GEN 2 FAULT.ALSO ON PFR TOO MANY FAULTS TO LIST! REF TSM 24-20-00-810-813 . CHECKED AIRCRAFT WIRING May 20, 2025 · N838UA · Airbus A319131 · AC Generator-AlternatorSDR CALA2025052104894Contactor · faultyGEN 2 FAILURE/TR2 FAILURE CAP REPORTED T/O INHIBIT OCCURRED DURING T/O FOLLOWED BY A TR2 FAULT AND GEN 2 FAULT. BOTH SCREENS ON FO SIDE BLANKED OUT. ABLE TO RECOVER GEN 2 BY CYCLING. TR2 FAULT REMAINS. PFR PIC ATTACHED. UPDATING TIME REF TSM 24-20-00-810-814 May 19, 2025 · N838UA · Airbus A319131 · AC Generator-AlternatorSDR CALA2025031402819Tape · peelingLOUD WHISTLE FM RH OVERWING EXIT EVEN AT 8 PSID FOUND PEELING SPEED TAPE FROM DIP TEMP REPAIR IN LP 4125574. REPLACED SPEED TAPE IAW SRM 57-41-11. OK TO CONTINUEMar 14, 2025 · N838UA · Airbus A319131 · Emergency ExitsSDR CALA2025031702870Tape · looseLOUD WHISTLING NOISE COMING FROM RH OVERWING EXI TS. NOISE STARTED JUST A FTER TAKEOFF FOUND TAPE LOOSE AREA ALREADY ON DIP LOG. 9620908 RE-SECURED WITH MISSING TAPE.Mar 13, 2025 · N838UA · Airbus A319131 · Emergency ExitsSDR CALA2025012902100Fuel Cap · missingPDA, FUELER REPORT FUEL CAP MISSING. INSTALLED NEW FUEL CAP IN REFERENCE TO AMM 28-25-41. OK TO CONTINUE. PARTS USED: 31-2825-9-0001,QTY :1 1339735,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1339735 SN OFF 1111 IPC REFERENCE # 28-00-00 CAP, COUPLINJan 29, 2025 · N838UA · Airbus A319131 · Fuel StorageSDR CALA2024120501412Battery · faultedEPSU BATTERY EMER R FAULT R/R EPSU BATTERY AT EPSU 12WL WITH A SERVICABLE UNIT FROM A/C 4046 REF AMM 33-51-38. OPS CHECKS OKDec 3, 2024 · N838UA · Airbus A319131 · Emergency LightingSDR CALA2024120401402Battery · failedOPERATIONAL CHECK OF CABIN EMERGENCY LIGHTS {A3NB-33-3-6012} - SYS OK LIGHT DOES NOT COME ON AFTER TEST. EPSU BATTERY AFT L 33-51-58. EPSU COMM AFT L. 33-51-38 R/R EPSU BATTERY AT EPSU 13WL WITH A SERVICABLE UNIT FROM A/C 4046 REF AMM 33-51-38. OPS CHECKS OKDec 2, 2024 · N838UA · Airbus A319131 · Emergency LightingSDR CALA2024082602266Support Frame · crackedR/H O/W EMERGENCY EXIT HAS CRACKS IN FRAME SUPPORT FWD & AFT, REMOVED & REPLACED R/H O/W EMERGENCY EXIT FWD & AFT FRAME SUPPOR TS IAW A319 SRM 51-72-11-911-001.Aug 19, 2024 · N838UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2024082602265Support Frame · crackedL/H O/W EMERGENCY EXIT HAS CRACKS IN AFT FRAME SUPPORT, REMOVED & REPLACED L/H O/W EMERGENCY AFT FRAME SUPPORT IAW A319 SRM 51-72-11-911-001 FRAME PN# D5227902620451 PO# 1145773.5,Aug 19, 2024 · N838UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2023122003687Skin · dentedAFT FUSELAGE TAIL SECTION FR73 STRINGER 30R-31R HAS INWARD DENT. THIS REPAIR IS CONSIDERED A CAT B REPAIR PER SRI 53-00-11-205-053. FABRICATED AND INSTALLED DOUBLER REPAIR AT FR73 STRINGER 30R-31R REPAIRED DENT TO AFT FUSELAGE TAIL SECTION, FR73 STRINGER CATDec 18, 2023 · N838UA · Airbus A319131 · Fuselage Main, Plate/SkinSDR CALA2022030100537Pump · failedYELLOW HYD RESV OVHTINFLIGHT. EMERGENCY RETURNED TO KDEN. OPERATED BOTH FWD AND AFT CARGO DOORS SEVERAL TIMES AND THE DOOR ENTERED ROTABLE PART INFO. SELECTOR SWITCHES RETURNED TO THE NEUTRAL POSITION EACH TIME ROTABLE PARTS CHANGE WAS INDICATED - TT # 1958381Mar 1, 2022 · N838UA · Airbus A319131 · Hydraulic Pump (Electric/Engine), MainSDR CALA2022011000098Probe · failedFUEL RT TANK OVERFLOW ECAM CAME ON TWICE AND BOTH TIMES CLEARED IT SELF WAS ON DURING EVENT WAS IAD TO LAX SO ASSUME FULL WING TANKS. FULL TANKS HUNTING MOST LIKELY CAUSE FOR "RT FUEL TANK OVERFLOW" MSG. MULTIPLE FAULTS FOR " RT QTY PROBE 28QT2" MULTIPLE LEGS.Jan 9, 2022 · N838UA · Airbus A319131 · Central WarningSDR CALA2021122002417Repair · noneREF DTA LP 7628364 AS PER ECRA 5331-02818 PART 1 STEP 3;PLANNING TO CONTACT ENGINEERING AFTER 09 OCTOBER 2022 BUT BEFORE 09 NOVEMBER 2022 FOR ECRA 5331-02818 PART 3 PERMAMANT REPAIR. REFERENCE ECRA 5331-02818 PART 1 STEP 3. BEFORE 09 NOVEMBER 2022 FOR ECRA 533Dec 20, 2021 · N838UA · Airbus A300* · Fuselage Structure (General)SDR CALA2021122002415Repair · noneACCOMPLISH A PERMANENT REPAIR PER PART 3 OF LATEST REVION OF ECRA 5331-02818 ON OR BEFORE 09 DECEMBER 2022. REF DTA LP 7037108 ACCOMPLISH PERMANENT REPAIR PER PART 3 OF LATEST REVISION OF ECRA 5331-02818 ON OR BEFORE 09 DECEMBER 2022. REF DTA LP7037108 ACCOMPLDec 20, 2021 · N838UA · Airbus A300* · Fuselage Structure (General)SDR CALA2021121202350Intercostal · cracked(REPAIR BEFORE NEXT FLT) ROTO PROBE OF RH FR16 #7 DOOR STOP FIT TING HOLES FOUND CRACKS IN THE I/B TOP AND I/B BOTTOM HOLES.() REPAIRED HOLES #1-3 FROM FRAME AND INTERCOASTAL DOOR STOP FITTIN G #7 FR16 LH IAW EA 319-5311-13-A2715, ECRA 5311-02680. EMP# V93 33Dec 12, 2021 · N838UA · Airbus A319131 · Fuselage Structure (General)SDR CALA2021121202345Bulkhead · cracked(AD 2019-20-10) LH FR16 DOOR STOP FITTING #7 HAS CRACK INDICATIO NS ON I/B TOP HOLE AND I/B BOTTOM HOLE. REPAIR BEFORE NEXT FLIGH T.() REPAIRED HOLES #1-3 FROM FRAME AND INTERCOASTAL DOOR STOP FITTIN BFM ON NR# 0017169 G #7 FR16 LH IAW A319-5311-13-A2731 AND CDec 11, 2021 · N838UA · Airbus A319131 · Fuselage Structure (General)SDR CALA2021121002338Antenna · corroded(A3NB-44-3-6004) GCS ANTENNA ADAPTER PLATE HAS EXFOLIATING CORRO SION CENTER AREA AFT ON ANTENNA. DOT 102-116.() GCS ANTENNA ADAPTER PLATE REPAIRED IAW EA 319-4420-13-A2749 REV'' _'' AND UAL EC/RA 5341-01290. NO DEVIATIONS EMP# V934344 WORK ACC OMPLISHED T ST Dec 10, 2021 · N838UA · Airbus A319131 · Fuselage Structure (General)SDR CALA2021121002337Fitting · cracked(REPAIR BEFORE NEXT FLT) ROTO PROBE OF RH FR16 #7 DOOR STOP FIT TING HOLES FOUND CRACKS IN THE I/B TOP AND I/B BOTTOM HOLES.() REPAIRED HOLES #1-3 FROM FRAME AND INTERCOASTAL DOOR STOP FITTIN G #7 FR16 LH IAW EA 319-5311-13-A2715, ECRA 5311-02680. EMP# V93 33Dec 10, 2021 · N838UA · Airbus A319131 · Fuselage Structure (General)SDR CALA2021121002336Fitting · cracked(AD 2019-20-10) LH FR16 DOOR STOP FITTING #7 HAS CRACK INDICATIO NS ON I/B TOP HOLE AND I/B BOTTOM HOLE. REPAIR BEFORE NEXT FLIGH T.() REPAIRED HOLES #1-3 FROM FRAME AND INTERCOASTAL DOOR STOP FITTIN BFM ON NR# 0017169 G #7 FR16 LH IAW A319-5311-13-A2731 AND CDec 10, 2021 · N838UA · Airbus A319131 · Standard Practices/StructuresSDR CALA2021112902186Stringer · corroded(A3NB-53-4-6179) AREA AFT OF BULK CARGO STRINGER BELOW OUTFLOW V ALVE IS CORRODED. DOT 102-130 () REMOVED & REPLACED STRINGER 31 R/H FR.64 TO FR67 R/H IAW SRM 51- 42-11. ACCOMPLISHED AT BFM ST AEROSPACE MOBILE. NR#0017016Nov 28, 2021 · N838UA · Airbus A319131 · Fuselage, Wing Attach FittingsSDR CALA2021112502170Stringer · corroded(A3NB-53-4-6179) AREA AFT OF BULK CARGO STRINGER BELOW OUTFLOW V ALVE IS CORRODED. DOT 102-130 () REMOVED & REPLACED STRINGER 31 R/H FR.64 TO FR67 R/H IAW SRM 51- 42-11. ACCOMPLISHED AT BFM ST AEROSPACE MOBILE. NR#0017016Nov 25, 2021 · N838UA · Airbus A319131 · Fuselage, Wing Attach FittingsSDR CALA2021111502097Beam · corroded(A3NB-53-3-6040), FWD PASSENGER CABIN FLOOR, MAIN STRUCTURE, BTW FR20-FR24 AT Y-1292, SEAT TRACK WITH CORROSION. DOT 88-001.() DAMAGE FOUND WITHOUT OF LIMITS IAW A319 SRM 53-00-15-283-001, RE PLACED PER NEW FLOOR BEAM P/N: D5311278220201 BATCH 0003778671, INSTNov 12, 2021 · N838UA · Airbus A319131 · Fuselage Structure (General)SDR CALA2021111102089Beam · corroded(A3NB-53-6102), FWD PASSENGER CABIN FLOOR, MAIN STRUCTURE, FROM FR25 AT Y-1292, SEAT TRACK WITH CORROSION. DOT 88-006() DAMAGE FOUND OUT OF LIMITS IAW A319 SRM 53-00-15-283-001, REPLAC ED PER NEW P/N: D5323345920000 BATCH: 00038644381, INSTALLED IAW A319 SRM 5Nov 11, 2021 · N838UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2021111002083Floorbeam · corroded(A3NB-53-3-6038), FWD PASSENGER CABIN FLOOR, MAIN STRUCTURE, FRO M FR14 TO FR20, BTW Y-254 AND Y254, STRUCTURE WITH CORROSION (2 PLACES) DOT 88-009() REMOVED AND REPLACED SEAT TRACK P/N: D5311146100200 AT FWD CABIN FLOOR Y-254, FR12-FR24 IAW SRM 51-42-11. SEE Nov 10, 2021 · N838UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2021111002082Seat Track · corroded(A3NB-53-3-6040), FWD PASSENGER CABIN FLOOR, MAIN STRUCTURE, BTW FR20-FR21 AT Y-765, SEAT TRACK WITH CORROSION. DOT 88-002() NEW SEAT TRACK INSTALLED IAW A-319 SRM 51-42-11/001 PARAGRAPH 2. E AND 2.F. EMP# V936039 WORK ACCOMPLISHED AT ST ENGINEERING AERO SPACENov 10, 2021 · N838UA · Airbus A319131 · Fuselage Structure (General)SDR CALA2021111002081Seat Track · corroded(A3NB-53-3-6038), FWD PASSENGER CABIN FLOOR, FR20, BTW FUSELAGE INNER SKIN AND SEAT TRACK AT Y-1292, STRUCTURE WITH CORROSION. D OT 88-010 () CORROSION FOUND OUT OF LIMITS IAW A319 SRM 53-11-14-283-007, REC EIVED NEW SUPPORT WEB P/N: D5311278520301 BATCH: 0003Nov 10, 2021 · N838UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2021110802062Seat Track · corroded(A3NB-53-3-6038), FWD PASSENGER CABIN FLOOR, MAIN STRUCTURE, FRO M FR14 TO FR20, BTW Y-254 AND Y254, STRUCTURE WITH CORROSION (2 PLACES) DOT 88-009() REMOVED AND REPLACED SEAT TRACK P/N: D5311146100200 AT FWD CABIN FLOOR Y-254, FR12-FR24 IAW SRM 51-42-11. SEE Nov 7, 2021 · N838UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2021110802061Seat Track · corroded(A3NB-53-3-6040), FWD PASSENGER CABIN FLOOR, MAIN STRUCTURE, BTW FR20-FR21 AT Y-765, SEAT TRACK WITH CORROSION. DOT 88-002() NEW SEAT TRACK INSTALLED IAW A-319 SRM 51-42-11/001 PARAGRAPH 2. E AND 2.F. EMP# V936039 WORK ACCOMPLISHED AT ST ENGINEERING AERO SPACENov 7, 2021 · N838UA · Airbus A319131 · Fuselage Structure (General)SDR CALA2021110802060Floor Support · corroded(A3NB-53-3-6038), FWD PASSENGER CABIN FLOOR, FR20, BTW FUSELAGE INNER SKIN AND SEAT TRACK AT Y-1292, STRUCTURE WITH CORROSION. D OT 88-010 () CORROSION FOUND OUT OF LIMITS IAW A319 SRM 53-11-14-283-007, REC EIVED NEW SUPPORT WEB P/N: D5311278520301 BATCH: 0003Nov 7, 2021 · N838UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2021110802044Beam · corroded(A3NB-53-3-6040), FWD PASSENGER CABIN FLOOR, MAIN STRUCTURE, BTW FR20-FR21 AT Y-254, SEAT TRACK WITH CORROSION. DOT 88-033() REMOVED AND REPLACED RAIL DUNMY Y-189 BETWEEN FR20 AND FR24 AT F WD PASSENGER CABIN FLOOR IAW SRM 51-42-11. EMP# V933866 WORK ACC OMPLINov 5, 2021 · N838UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2021110802043Beam · corroded(A3NB-53-3-6187), AFT PASSENGER CABIN FLOOR, MAINSTRUCTURE BTW F R66 AND FR68, LONGERON BEAM WITH CORROSION (5 PLACES) DOT 88-015 () LONGERON BEAM REPLACED IAW A319 SRM 51-42-11/001 PARAGRAPH 2.E A ND 2.F. FORM 44-0008 ATTACHED EMP# V933870 WORK ACCOMPLISHED ANov 5, 2021 · N838UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2021102901988Beam · corroded(A3NB-53-3-6187) CABIN FLOOR STRUCTURE FR 66 Y765 HAS CORROSION AT 2 SPOTS. DOT NO 17-25() REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS ON HARD POINT AREA IAW SRM 51-74-00. REMOVED AND REPLACED PN# D534 720900200 BATCH# 0008380224 IAW SRM 51-4Oct 27, 2021 · N838UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2018062101452Door Sill · corrodedR2 DOOR SILL HAD CORROSION, AFT OF FRAME 66. REMOVED AND REPLACED THE R2 DOOR SILL IAW SRM 51-42-11.Jun 10, 2018 · N838UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2018012600345Light · detachedSEAT 30C EMERGENCY LIGHT DETACKED. INSTALLED THE LIGHT. OPS OKJan 26, 2018 · N838UA · Airbus A319131 · Emergency LightingSDR CALA2017123104708Actuator · faultyF/CTL SLATS FAULT DISPLAYED. EMERGENCY DECLARED. FOUND LT NR 4 SLAT TRANSMISSION TORQUE LIMITER TRIPPED. REPLACED PER AMM27-84-49-000-002-A AND 27-84-49-400-002-A FOR TYPE B ACTUATOR. ALL OTHER TRANSMISSION FOUND OK. SLAT SYS OPS CHECKS OK. CA T CHK ACP ALL CHDec 31, 2017 · N838UA · Airbus A319131 · Leading Edge Slat ActuatorSDR CALA2017123004688Computer · faultyFLT CONTROLS, SLATS FAULT DISPLAYED. EMERGENCY DECLARED. REMOVED AND REPLACED THE SFCC NR 1 AND 2 IAW AMM 27-5 1-34. ACCOMPLISHED BITE TEST IAW AMM 27-51-00-740-002-A, BITE TEST IAW AMM 27-81-00-740-002-A, OPS TESTED IAW AMM TASK 27-54-00-710 -002-A AND CAT Dec 30, 2017 · N838UA · Airbus A319131 · Leading Edge Slat Control SystemSDR CALA2017103003872Battery · faultedDURING 2SVC CHK, FOUND FAULT DURING THE CABIN EMERGENCY LIGHTS OPERATIONAL TEST, SYSTEM FAULT ''EPSU BATTERY FWD LEFT". PERFORMED OPERATIONAL CHECK OF ESS ALL CHECKS NORMAL NO FAULTS FOUND REF AMM 33-51-38.Oct 30, 2017 · N838UA · Airbus A319131 · Emergency LightingSDR CALA2017090303040Battery Pack · inoperativeEMERGENCY LIGHT TEST FAILED AT PTP PANEL. REPLACED THE BATTERY AT EPSU 13WL IAW AMM 33-51-38. OK FOR SERVICESep 3, 2017 · N838UA · Airbus A319131 · Emergency LightingSDR CALA2017060501727Lens · missing1L EXIT DOOR LIGHT LENS MISSING. REPLACED THE LENS.Jun 5, 2017 · N838UA · Airbus A319131 · Emergency LightingSDR CALA2017052201534Slide · crackedLT OVERWING SLIDE HAS 2 EACH CRACKS IN AREA 2 THAT EXTEND PAST LIMITS REF MM 25-62-42-210-002. REPLACED LT OVERWING ESCAPE SLIDE REF AMM25-62-42.May 22, 2017 · N838UA · Airbus A319131 · Escape SlideSDR CALA2017050101227Power Supply · no testDURING TEST OF EMERGENCY BATTERIES, THE EPSU BATTERY AFT LT FAILED TO TEST. REPLACED EMERGENCY POWER SUPPLY. OPS CHECKED OK.May 1, 2017 · N838UA · Airbus A319131 · Emergency LightingSDR CALA2017022400445Skin · dentedDENT IN RIGHT FORWARD FUSELAGE JUST BELOW AND FORWARD OF DOOR 1R. REPAIRED DENT IN FUSELAGE PER ECRA 5311-01852. ACP PERM REPAIR IN 335D OR 20 FEB 2018 TOMC-APPROVAL. ACCOMPLISH A PERMANENT REPAIR AT FR12-13 RT FUSELAGE SKIN JUST BELOW THE Z-520 FLOOR LEVEL PEFeb 21, 2017 · N838UA · Airbus A319131 · Fuselage Main, Plate/SkinSDR CALA2016061595458Keelbeam · damagedDAMAGED HOLES ON KEELBEAM FOUND DURING ACP OF FCD 5330-05575, REV A. ALL HOLES REPAIRED IAW ECRA 5330-05726.Jun 14, 2016 · N838UA · Airbus A319131 · Fuselage Main, Keel
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