# Service difficulty reports: N837UA

A list on [N837UA](https://openairdocs.org/aircraft/N837UA.md).

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

Page 1 of 3 · 139 reports

- [SDR CALA2026101620404](https://openairdocs.org/sdr/CALA2026101620404.md): Pump · leaking · Oct 14, 2026 · N837UA · Airbus A319131 · Hydraulic Pump (Electric/Engine), Main
  > HYD G ENG 1 PUMP LO PR, HYD G SYS LO PR, GREEN SYS DEPLETED SDR INFO ADDED FOUND AN ACTIVE LEAK WITH HYD PRESSURE OFF ON LINE AT THE TOP OF NR 1 ENGINE OTBD SIDE. JUST BEHIND THE PYLON INTERFACE BRACKET. REPLACED DAMAGED PYLON HYDRAULIC LINE ON #1 ENGINE REF
- [SDR CALA2026041415358](https://openairdocs.org/sdr/CALA2026041415358.md): Filter · dirty · Apr 10, 2026 · N837UA · Airbus A319131 · Air Distribution System
  > CABIN RE-CIRCULATION FILTERS NEEDS TO BE REPLACE WITHIN 2 DAYS REF LOG# 8508734 CABIN RE-CIRCULATION FILTERS TO BE REPLACEWITHIN 2 DAYMM 05-51-10-200-801-C1 NO ODOR OBSERVED OR ABLE TS REF AO BE IDENTIFIED BY MX. RECIRC FILTERS REQUIRE REPLACEMENT WITHIN 2 DAY
- [SDR CALA2026030214202](https://openairdocs.org/sdr/CALA2026030214202.md): Pressure Switch · damaged · Feb 28, 2026 · N837UA · Airbus A319131 · Hydraulic System, Auxiliary
  > AFTER RAT FAN BLADE INSPECTION RED LIGHT ACTUATOR PRESSURE LGHT IS ILLUMINATED ON RAT CONTROL MODULE AFTER STOWING RAT ALSO RAT FAULT DISPLAYED ON UPPER ECAM WITH AMBER TRIANGLE DISPLAYED ON HYDRAULICS PAGE. REPLACED RAT ACTUATOR PRESURE SWITCH, LEAK CK OK OPS
- [SDR CALA2026021813891](https://openairdocs.org/sdr/CALA2026021813891.md): Light · inoperative · Feb 18, 2026 · N837UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY LIGHTS AT SEAT 25C INOPERATIVE. REPLACED THE LIGHT ASSY IAW AMM 33-51-19. OPS CHECKED GOOD.
- [SDR CALA2025082608123](https://openairdocs.org/sdr/CALA2025082608123.md): Fuel Cap · missing · Aug 24, 2025 · N837UA · Airbus A319131 · Fuel Storage
  > RAMP REPORT OF FUEL COUPLING CAP MISSING. RIGHT WING. INSTALLED FUEL CAP IAW AMM 28-25-41-400-005-A, SUB TASK 28-25-41-420-056-C, FROM STEP B2N TO B2Q,
- [SDR CALA2025062505856](https://openairdocs.org/sdr/CALA2025062505856.md): Slide · faulted · Jun 22, 2025 · N837UA · Airbus A319131 · Escape Slide
  > PLEASE CHECK THE SLIDE PRESSURE GAUGE AT DOOR 2L AND REPLACE SLIDE IF THE NEEDLE IS IN AREA B CARRIED BY ELB ORIGINAL CYCLES LIMIT OF: 001 EXTENDED BY 001 NEW TIME REMAINING 001. REMOVED AND REPLACED DOOR 2 LEFT EVACUATION SLIDE REF 25-62-44. OPS CHECK SATI
- [SDR CALA2025062505855](https://openairdocs.org/sdr/CALA2025062505855.md): Gauge · no discrepancy · Jun 22, 2025 · N837UA · Airbus A319131 · Emergency Equipment
  > FA REPORTS DOOR 2L PRESSURE GAUGE IN RED. INSPECTED GAUGE PER AMM 25-62-00. SLIDE PRESSURE IS WITHIN AMM LIMITS. INSPECTED GAUGE PER AMM 25-62-00. SLIDE PRESSURE IS WITHIN AMM LIMITS.
- [SDR CALA2025060205157](https://openairdocs.org/sdr/CALA2025060205157.md): Light · disconnected · May 30, 2025 · N837UA · Airbus A319131 · Light System Wiring
  > SEAT 23ABC EMERGENCY PATHWAY LIGHT FOUND INOP. REPLACED LENS COVER AND RECONNECTED EMERGENCY LIGHT AT SEAT 23ABC PER AIRBUS 319/320 AMM 33-51-19. OPS CHECK GOOD
- [SDR CALA2025051404662](https://openairdocs.org/sdr/CALA2025051404662.md): Bottle · no discrepancy · May 10, 2025 · N837UA · Airbus A319131 · Escape Slide
  > FA REPORTS DOOR 2L SLIDE PRESSURE GUAGE IN RED. INDICATOR NEEDLE IS ONE NEEDLE WIDTH OVER THE GREEN BAND TO THE HIGH SIDE INTO THE RED ALLOWED TEMPERTURE CONDITIONS TO STABILIZE. PRESSURE INDICATION IS IN AREA A BAND. PER AMM TASK 25-62-00-210-001-A. OKAY FOR
- [SDR CALA2025050604498](https://openairdocs.org/sdr/CALA2025050604498.md): Slide · none · May 3, 2025 · N837UA · Airbus A319131 · Escape Slide
  > L2 DOOR PRESSURE GAUGE SHOWS OVER PRESSURE SLIDE PRESSURE INDICATION FALLS WITHIN SERVICEABLE LIMITS. REF AMM 25-62-00-210- 001-A.
- [SDR CALA2025032703256](https://openairdocs.org/sdr/CALA2025032703256.md): Eec · faulted · Mar 24, 2025 · N837UA · Airbus A319131 · Fuel Controlling System
  > ENG 2 COMPRESSOR STALL A T CRZ ALT FL370 ENG 2 STALL ECAM ENG 2 EPR MODE FAULT CREW REPORTED MULTIPLE LOUD BANGS FOLLOWED BY STALL AND EPR MODE ECAM, ENGINE WAS REDUCED TO IDLE & RAN REMAINDER OF FLIGHT AT IDLE. CREW REPORTED ONE MORE LOUD BANG AFTER LANDING P
- [SDR CALA2025020502215](https://openairdocs.org/sdr/CALA2025020502215.md): Vsv · failed · Feb 3, 2025 · N837UA · Airbus A319131 · Fuel Controlling System
  > ENG2 FAIL ON T/O ROLL. NO INDICATION NOTICED PRIOR TO FAILURE ENG 2 STALL WITH CFDS VSV MECH/BLD VLV/LPC2 REFERENCE TSM 71-00-00-810-809-A, ALSO SUGGEST MCD INSPECTION PER AMM 79-22-45-000-010-A TO DETERMINE ENGINE SERVICEABILITY. TOMC-MEREDITH FLAGGING SDR
- [SDR CALA2025020502214](https://openairdocs.org/sdr/CALA2025020502214.md): Slide · no test · Feb 2, 2025 · N837UA · Airbus A319131 · Escape Slide
  > DOOR 2 LEFT SLIDE DID NOT DEPLOY PROPERLY. REMOVED L2 SLIDE IAW AMM 25-62-44/401. INFO ONLY... PER FIRE DEPT, L2 SLIDE DID INFLATE AND 3 PASSENGERS WENT DOWN UNTIL IT DEFLATED AND FLIGHT ATTENDANT KEPT PEOPLE FROM USING IT.
- [SDR CALA2025012802086](https://openairdocs.org/sdr/CALA2025012802086.md): Sdac · unknown · Jan 28, 2025 · N837UA · Airbus A319131 · Hydraulic System, Main
  > HYD G RSVR OVHT. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN. UPDATED MA
- [SDR CALA2024101102628](https://openairdocs.org/sdr/CALA2024101102628.md): Frame · cracked · Oct 9, 2024 · N837UA · Airbus A319131 · Fuselage Main, Frame
  > RH FR16 DOUBLE JOGGLE HOLES FOUND CRACKED, REQUIRING PARTIAL FRAME REPLACEMENT AT C CK IN BFM AS NOTED ON N/R''S 110289 &; 110293. 1, PART 1.2 REQUIRES DIP AS FOLLOWS; ACCOMPLISH INITIAL INSPS A ST REV OF ECRA5311-03281 ON/BEFORE ACFT REACHES 37002 TTL FC (FH
- [SDR CALA2024101102627](https://openairdocs.org/sdr/CALA2024101102627.md): Frame · cracked · Sep 13, 2024 · N837UA · Airbus A319131 · Fuselage Main, Frame
  > (SUPPORT TASK) DURING ROTO TEST OF RH FRAME 16 HOLE 6 FOUND CRAC KED IN FRAME LAYER AT THE 3:00 POSITION. REPAIR BEFORE NEXT FLIG HT.() TRANSFERRED REPAIR INFORMATION AND DIP REQUIREMENTS TO LP''S 9509350, 9509474 & 9509861. THIS ITEM CAN BE CLEARED.
- [SDR CALA2024083000521](https://openairdocs.org/sdr/CALA2024083000521.md): Seal · missing · Aug 26, 2024 · N837UA · Airbus A319131 · Trailing Edge Flaps
  > PDA 2 RH OB FLAP IB CUSHION SEAL AND PLATE MISSING FROM AIRCRAFT UPON ARRIVAL. 55SQ IN. UPDATED SDR INFORMATION.
- [SDR CALA2022060101415](https://openairdocs.org/sdr/CALA2022060101415.md): Hydraulic Line · leaking · Jun 1, 2022 · N837UA · Airbus A319131 · Hydraulic Pump (Electric/Engine), Main
  > HYD Y ENG2 PUMP LOPRESSURE PILOT SAID PARKING BRAKE INOP DUE TO LOW PRESS,FOUND LARGE HYD LEAK UNDER ENG 2 ALSO GREEN SYST HYD AND YELLOW HYD LOW. 29-13-00-810-804-A UPON INSPECTION FOUND HYDRAULIC LINE TO THE HCU AT 12 O CLOCK R/R PER AMM 29-13-51-400-010-
- [SDR CALA2022032800811](https://openairdocs.org/sdr/CALA2022032800811.md): Accumulator · leaking · Mar 28, 2022 · N837UA · Airbus A319131 · Hydraulic Pump (Electric/Engine), Main
  > CREW REPORTS HYD Y RSVR LO LVL MESSAGE. CREW FOLLOWED QRH 130.44 PTU SWITCHED OFF AND ENG 2 HYD PUMP SWITCHED OFF. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN UPDATED MAA CODE FIX USING VENDOR MAA SCREEN MAC METER INITIATED FOR WITH VENDOR ID V928786 PLEASE C
- [SDR CALA2022022800520](https://openairdocs.org/sdr/CALA2022022800520.md): Reservoir · none · Feb 28, 2022 · N837UA · Airbus A319131 · Hydraulic Power Accumulator, Main
  > ABOUT/40 MINT AFTER T/OGOT G RSVR OVHT ECAM.WHEN OVHT OUT G ENG PUMP+ PTU ON GOT AIRFRM.FLIGHT CREW TURNED THE GREEN HYD ENG PUMP AND THE PTU BACK ON. AND GREEN HYD SYSTEM OVERHEAT DID NOT COME BACK ON. SEEMED SUSPICIOUS. WITH LEFT ENGINE RUNNING, PTU OPERATED
- [SDR CALA2022021600399](https://openairdocs.org/sdr/CALA2022021600399.md): Drain Mast · clogged · Feb 15, 2022 · N837UA · Airbus A319131 · Water and Waste System
  > REF L/P 7964207- AFT GALLEY DRAIN CLOGGED AND LEAKING. SPILL CLEANUP REQUIRED. CABIN FLOOR FRAME 62 THUR 66 (CTR AISLE ROW 32 TO AFT GALLEY). NO WATER IN AFT CARGO COMPT DETECTED. PLACED ON DIP. WITHIN 7 DAYS, ACCOMPLISH ECRA 2011-01000, GALLEY SPILL, SECTION
- [SDR CALA2022020100282](https://openairdocs.org/sdr/CALA2022020100282.md): Control Unit · unserviceable · Jan 31, 2022 · N837UA · Airbus A319131 · Landing Gear System
  > BRAKE SYS 1 FAULT, SYS RESET THEN FAULT CAME BACK LOCKED FOR FIX ITEM UNLOCKED FOR CLEARING ACTION. REMOVED AND REPLACED #1 BSCU PER AMM 32-42-34-400AND TESTED OK, LAND VERIFY PASSED. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1248627 SN OFF 5694 UNIT, BRAKE S
- [SDR CALA2022012000197](https://openairdocs.org/sdr/CALA2022012000197.md): Keelbeam · elongated · Jan 20, 2022 · N837UA · Airbus A319131 · Vertical Stabilizer
  > WHILE ACCOMPLISHING FCD 5330-05575 RH HOLES, FOUND ALL HOLES OUT OF SIDE LIMITS AND ELONGATED WITH VISUAL DAMAGE EXCEPT HOLES #R 13 AND #R19. REPAIRED RH KEEL BEAM FASTENER HOLE AND FITTING IAW EC/RA 5330-0 6891. EMP: V935774 WC: 0018386 STA: ST ENG BFM SFR# 1
- [SDR CALA2022012000195](https://openairdocs.org/sdr/CALA2022012000195.md): Fastener · cracked · Jan 20, 2022 · N837UA · Airbus A319131 · Fuselage Main, Frame
  > (SDR) DOUBLE JOGGLE FASTENER HOLES LH FR16 TOP HOLES AFT ROW, HO LE B HAS A CRACK INDICATION, MUST BE REPAIRED BEFORE NEXT FLIGHT PER EA 5311-02442. REPAIRED LH FR16 HOLE B DOUBLE JOGGLE IAW EC/RA 5311-02735. SEE DTA DIP #7806847 FOR INSPECTION REQUIREMENTS. E
- [SDR CALA2022012000194](https://openairdocs.org/sdr/CALA2022012000194.md): Keelbeam · elongated · Jan 20, 2022 · N837UA · Airbus A319131 · Vertical Stabilizer
  > WHILE ACCOMPLISHING FCD 5330-05575 LH HOLES, FOUND ALL HOLES OUT OF SIDE LIMITS AND ELONGATED WITH VISUAL DAMAGE (NO DOT) REPAIRED LH KEEL BEAM FASTENER HOLES AND FITTINGS IAW EC/RA 5330 -06891 EMP: V935774 WC: 0018385 STA: ST ENT BFM SFR# 1027501
- [SDR CALA2022011800184](https://openairdocs.org/sdr/CALA2022011800184.md): Keelbeam · elongated · Jan 18, 2022 · N837UA · Airbus A319131 · Fuselage Structure (General)
  > WHILE ACCOMPLISHING INSPECTIONS PER FCD 5330-05575D OF THE RH FUSELAGE KEEL BEAM MLG ATTACHMENT STRUCTURE, PRODUCTION REPORTED ALL HOLES OUT OF LIMITS AND ELONGATED. -06891 (SEE FIGURE 1 - 17 OF EC/RA 5311-02712 FOR LOCATIONS). ACCOMPLISH A PERMANENT REPAIR PE
- [SDR CALA2022011800179](https://openairdocs.org/sdr/CALA2022011800179.md): Keelbeam · elongated · Jan 18, 2022 · N837UA · Airbus A319131 · Fuselage Main, Keel
  > WHILE ACCOMPLISHING INSPECTIONS PER FCD 5330-05575D OF THE LH FUSELAGE KEEL BEAM MLG ATTACHMENT STRUCTURE, PRODUCTION REPORTED ALL HOLES OUT OF LIMITS AND ELONGATED. 02712. (SEE FIGURE 1 - 17 OF EC/RA 5311-02712 FOR LOCATIONS). ACCOMPLISH A PERMANENT REPAIR PE
- [SDR CALA2022011800176](https://openairdocs.org/sdr/CALA2022011800176.md): Frame · cracked · Jan 18, 2022 · N837UA · Airbus A319131 · Fuselage Main, Frame
  > DOUBLE JOGGLE FASTENER HOLES LH FR16 TOP HOLES AFT ROW. HOLE B H AS A CRACK INDICATION. MUST BE REPAIRED BEFORE NEXT FLIGHT PER E A 5311-02442. WITH EC/RA 5311-02735. WORK ACCOMPLISHED BY VTMAE EMPLOYEE AIRCRAFT FLIGHT CYCLES, AND AT INTERVALS NOT TO EXCEED 4,
- [SDR CALA2022011800175](https://openairdocs.org/sdr/CALA2022011800175.md): Rib · elongated · Jan 18, 2022 · N837UA · Airbus A319131 · Fuselage Structure (General)
  > WHILE ACCOMPLISHING FCD 5330-05575 LH HOLES, FOUND ALL HOLES OUT OF SIDE LIMITS AND ELONGATED WITH VISUAL DAMAGE (NO DOT)
- [SDR CALA2022011800174](https://openairdocs.org/sdr/CALA2022011800174.md): Rib · elongated · Jan 18, 2022 · N837UA · Airbus A319131 · Fuselage Structure (General)
  > WHILE ACCOMPLISHING FCD 5330-05575 RH HOLES, FOUND ALL HOLES OUT OF SIDE LIMITS AND ELONGATED WITH VISUAL DAMAGE EXCEPT HOLES #R 13 AND #R19.
- [SDR CALA2022011700164](https://openairdocs.org/sdr/CALA2022011700164.md): Stop Fitting · cracked · Jan 16, 2022 · N837UA · Airbus A319131 · Fuselage Structure (General)
  > RH FR16 DOORSTOP #7 HAS CRACK INDICATIONS. ACCOMPLISHED BY VTMAE EMPLOYEE V935774. ACCOMPLISH EC/RA 5311-02712 ON OR BEFORE THE AIRCRAFT REACHES 40,251 INTERVALS NOT TO EXCEED 15,500 FLIGHT CYCLES THEREAFTER. INSPECTION REQUIREMENTS PER PART 2A OF LATEST REVIS
- [SDR CALA2022011700163](https://openairdocs.org/sdr/CALA2022011700163.md): Fastener · cracked · Jan 16, 2022 · N837UA · Airbus A319131 · Fuselage Main, Frame
  > DOUBLE JOGGLE FASTENER HOLES LHFR20 TOP HOLES AFT ROW, HOLE A HA S A CRACK INDICATION, MUST BE REPAIRED BEFORE NEXT FLIGHT PER EA 5311-02442. REPAIRED L/H FR20 DOUBLE JOGGLE FASTENER HOLES IAW EC/RA 5311-02 726. SEE DTA DIP LP# 7802054 FOR INSPECTION REQUIREME
- [SDR CALA2022011400144](https://openairdocs.org/sdr/CALA2022011400144.md): Pressure Panel · cracked · Jan 13, 2022 · N837UA · Airbus A319131 · Fuselage Structure (General)
  > CRACK INDICATIONS NOTED AT LEFT FR36 PRESSURE PANEL HOLES #3 THRU #9. PER ECRA 5330-06903. WORK ACCOMPLISHED BY V935774 TOTAL AIRCRAFT FLIGHT CYCLES, OR 128,977 TOTAL PERFORM AN INSPECTION PER PART 2 OF THE LATEST REF LP 7800794. UPON THE ACCUMULATION OF 60,65
- [SDR CALA2022011400142](https://openairdocs.org/sdr/CALA2022011400142.md): Frame · cracked · Jan 13, 2022 · N837UA · Airbus A319131 · Fuselage Structure (General)
  > LH FRAME 20 DOUBLE JOGGLE HOLE "A" CRACKED 5311-02726. WORK ACCOMPLISHED BY VTMAE EMP V935774. ON OR CYCLES, AND AT INTERVALS NOT TO EXCEED 5,900 FLIGHT CYCLES, REVISION OF ECRA 5311-02726. BEFORE THE ACCUMULATION OF 35,451 TOTAL AIRCRAFT FLIGHT THEREAFTER, P
- [SDR CALA2022011400134](https://openairdocs.org/sdr/CALA2022011400134.md): Intercostal · cracked · Jan 13, 2022 · N837UA · Airbus A319131 · Fuselage Main, Structure
  > ROTO PROBE OF RH FR20 #7 DOOR STOP FITTING FOUND THAT THE BOTTOM IB HOLE HAS A CRACK INDICATION 001/002. WORK ACCOMPLISHED BY VTMAE EMP V935774 ACCOMPLISH EC/RA 5311-02712 ON OR BEFORE THE AIRCRAFT REACHES 40,251 TOTAL EXCEED 15,500 FLIGHT CYCLES THEREAFTER. I
- [SDR CALA2022011400133](https://openairdocs.org/sdr/CALA2022011400133.md): Frame · cracked · Jan 13, 2022 · N837UA · Airbus A319131 · Fuselage Main, Frame
  > DOUBLE JOGGLE FASTENER HOLES LHFR20 TOP HOLES AFT ROW, HOLE A HA S A CRACK INDICATION, MUST BE REPAIRED BEFORE NEXT FLIGHT PER EA 5311-02442.
- [SDR CALA2022011400136](https://openairdocs.org/sdr/CALA2022011400136.md): Frame · cracked · Jan 13, 2022 · N837UA · Airbus A300* · Fuselage Main, Structure
  > LH FR16 #1 DOOR STOP FITTING ROTO PROBE FOUND THAT THE BOTTOM IB HOLE HAS A CRACK INDICATION 001/002. WORK ACCOMPLISHED BY VTMAE EMP V935774 ACCOMPLISH EC/RA 5311-02712 ON OR BEFORE THE AIRCRAFT REACHES 40,251 TOTAL EXCEED 13,700 FLIGHT CYCLES THEREAFTER. INSP
- [SDR CALA2022011400135](https://openairdocs.org/sdr/CALA2022011400135.md): Frame · cracked · Jan 13, 2022 · N837UA · Airbus A300* · Fuselage Main, Structure
  > LH FR35 ROTO PROBE AT STGR 30 FASTENER HOLES FOUND THE BOTTOM AF T HOLE CRACKED ACCOMPLISHED BY VTMAE EMP V935774 ON OR BEFORE JUNE 20, OF ECRA5310-07963 2022, PERFORM AN INSPECTION PER PART 2 OF THE LATEST REVISION PERFORMED INTERIM REPAIR TO LH FR35 STGR 30
- [SDR CALA2022011400124](https://openairdocs.org/sdr/CALA2022011400124.md): Actuator · failed insp · Jan 12, 2022 · N837UA · Airbus A300* · Doors
  > R1 DOOR DAMPER FAILED OPS CHECK
- [SDR CALA2022011300123](https://openairdocs.org/sdr/CALA2022011300123.md): Frame · cracked · Jan 12, 2022 · N837UA · Airbus A300* · Fuselage Main, Structure
  > TWO ADDTIONAL FASTENER HOLES WERE FOUND CRACKED AT FR36 PRESSURE PANEL O/B OF ALLOWABLE CUT-OUT AREA REPAIRED ADDITIONAL FASTENER HOLES FOUND CRACK AT FR36 PRESSURE PANEL IAW EC/RA 5330-01903. EMP: V935774 WC: 0018304 STA: ST ENG BFM SFR# 1027449
- [SDR CALA2022011300122](https://openairdocs.org/sdr/CALA2022011300122.md): Intercostal · cracked · Jan 12, 2022 · N837UA · Airbus A300* · Fuselage Main, Structure
  > RH FR16 #1 DOOR STOP FITTING ROTO PROBE FOUND THAT THE BOTTOM IB HOLE HAS A CRACK INDICATION REPAIRED RH FR16 #1 DOOR STOP FITTING AREA IAW EC/RA 5311-02712. EMP: V935774 WC: 0017897 STA: ST ENG BFM SFR# 0017897
- [SDR CALA2022011300121](https://openairdocs.org/sdr/CALA2022011300121.md): Frame · cracked · Jan 12, 2022 · N837UA · Airbus A300* · Fuselage Main, Structure
  > RH FR16 #7 DOOR STOP ROTO PROBE FOUND THAT THE TOP IB AND BOTTOM IB HOLES HAVE CRACK INDICATIONS REPAIRED RH FR16 #7 DOOR STOP FITTING AREA IAW EC/RA 5311-02712. EMP: V935774 WC: 0017896 STA: ST ENG BFM SFR# 1027447
- [SDR CALA2021122002414](https://openairdocs.org/sdr/CALA2021122002414.md): Beam · corroded · Dec 20, 2021 · N837UA · Airbus A300* · Fuselage Main, Frame
  > FWD CABIN, FLOOR BEAM Y254 BETWEEN FR16/20 HAS CORROSION. REMOVED FLOOR BEAM Y254 BETWEEN FR16 AND FR20 CORROSION AROUND T D5311281820401 IAW SRM 51-42-11. EMP: V933870 WC: 0018103 STA: S HE SELF-LOCKING CLIP NUT IS NOT PERMITTED IAW SRM 53-11-14-283-0 T ENG B
- [SDR CALA2021122002412](https://openairdocs.org/sdr/CALA2021122002412.md): Frame · gouged · Dec 20, 2021 · N837UA · Airbus A300* · Fuselage, Wing Attach Fittings
  > CABIN FLOOR STRUCTURE FRAME HAS GOUGE AT FRAME 68 Y1292 REMOVED CORROSION CABIN FLOOR STRUCTURE FR68 Y1292 BEAM IAW SRM BFM SFR# 1027223 51-74-00 BLENDED AREA MEASURES L=1.5" W=1.250" D=0.019" ORIGINAL THICKNESS 0/155" REMAINING THICKNESS 0.136" FOUND OUT OF L
- [SDR CALA2021121702388](https://openairdocs.org/sdr/CALA2021121702388.md): None · corroded · Dec 17, 2021 · N837UA · Airbus A319131 · Fuselage, Wing Attach Fittings
  > CABIN FLOOR STRUCTURE FRAME HAS CORROSION AT FRAME 65 Y765 REMOVED CORROSION ON CABIN STRUCTURE FLOOR BEAM Y765 AT FRAME 65 51-72-11-911 AND 51-42-11. EMP: V933866 WC: 0018116 STA: ST ENG IAW SRM 51-74-00. FRAME FOUND OUT OF LIMITS IAW SRM 53-00-14-28 BFM SFR#
- [SDR CALA2021121702384](https://openairdocs.org/sdr/CALA2021121702384.md): Beam · corroded · Dec 16, 2021 · N837UA · Airbus A319131 · Fuselage Main, Frame
  > FWD CABIN, FLOOR BEAM Y254 BETWEEN FR16/20 HAS CORROSION.
- [SDR CALA2021121702383](https://openairdocs.org/sdr/CALA2021121702383.md): Beam · gouged · Dec 16, 2021 · N837UA · Airbus A319131 · Fuselage, Wing Attach Fittings
  > CABIN FLOOR STRUCTURE FRAME HAS GOUGE AT FRAME 68 Y1292
- [SDR CALA2021121402364](https://openairdocs.org/sdr/CALA2021121402364.md): Beam · corroded · Dec 14, 2021 · N837UA · Airbus A319131 · Fuselage, Wing Attach Fittings
  > CABIN FLOOR STRUCTURE FRAME HAS CORROSION AT FRAME 65 Y765
- [SDR CALA2021121202349](https://openairdocs.org/sdr/CALA2021121202349.md): Floor Support · elongated · Dec 12, 2021 · N837UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT CABIN, LH DOOR SILL FLANGE FR67-FR68 NUT PLATE HOLE IS ELONG ATED
- [SDR CALA2021121202343](https://openairdocs.org/sdr/CALA2021121202343.md): Beam · corroded · Dec 10, 2021 · N837UA · Airbus A319131 · Fuselage, Wing Attach Fittings
  > CABIN FLOOR STRUCTURE FRAME HAS CORROSION AT FRAME 68 Y765 REMOVED CORROSION ON CABIN FLOOR STRUCTURE FRAME Y765 FR68 IAW S -11-911 AND 51-42-11. EMP: V933866 WC: 0018126 STA: ST ENG BFM S RM 51-74-00. FRAME FOUND OUT OF LIMITS. ORIGINAL THICKNESS 0.160 FR# 10

Next page: https://openairdocs.org/aircraft/N837UA/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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 = 'N837UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N837UA/reports

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