# Service difficulty reports: N897UA

A list on [N897UA](https://openairdocs.org/aircraft/N897UA.md).

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

- [SDR CALA2026052016403](https://openairdocs.org/sdr/CALA2026052016403.md): Slide · faulted · May 19, 2026 · N897UA · Airbus A319132 · Escape Slide
  > R2 DOOR SLIDE/RAFT CANNOT BE SAFETIED. DEPLOYED R2 RAFT IAW AMM 25-62-00-710-001-A & EC/RA 2562-01 231. REMOVED AND REPLACED RAFT IAW AMM 25-62-44-000-805-A & 25-62-44-400-803-A. REPLACED DAMPER DIAPHRAGM IAW AMM 52-1 0-00-610-001-A. OPS CHECK OF EPSU AND RE
- [SDR CALA2026042415696](https://openairdocs.org/sdr/CALA2026042415696.md): Fan · faulted · Apr 22, 2026 · N897UA · Airbus A319132 · Air Distribution Fan
  > AVIONIC VENT BLOWER FAN C/B (AD 10) POPPED ON 123VU PANEL.T/S POPPED BREAKER BY REMOVING AVIONICS VENT FAN 20HG CONNECTOR AND JUMPERING PINS D&E. BREAKER STAYED IN. CHECKED FOR 115VAC AT PINS J,K,&L. PIN L ONLY HAD 8VAC. WENT TO RELAY 8HQ ON THE 107VU PANEL AN
- [SDR CALA2025110310842](https://openairdocs.org/sdr/CALA2025110310842.md): Elec Connector · damaged · Oct 31, 2025 · N897UA · Airbus A319132 · Light System Wiring
  > EMERGENCY FLOOR PROXIMITY LIGHTS INOP AT SEATS 28A AND 29A. FOUND WIRE DISCONNECTED FROM PLUG CONNECTOR, REPINNED, INSTALLED AND RECONNECT PLUG PER ESPM 20-48-27 OPS. CHECK GOOD ON CABIN EMERGENCY LIGHTING SYS. PER A.M.M. 33-51-00-710-805-A
- [SDR CALA2025090408446](https://openairdocs.org/sdr/CALA2025090408446.md): Proximity Switch · out of limits · Aug 29, 2025 · N897UA · Airbus A319132 · Door Warning System
  > DOOR AFT CARGO ECAM MSG SHORTLYT AFTER TAKEOFF. ACFT HAS PREVIOU S HISTORY. CHECKED WIRES WITHIN HARNESS 4613VB. ALSO SEE MX TIP 52-019 T/S PER AMM 32-31-00-810-886, 32WW PROXIMITY SENSOR GAP WITHIN LIMIT PER AMM 52-71-00-820-003. PERFORMED WIRING CHECK W
- [SDR CALA2025090108320](https://openairdocs.org/sdr/CALA2025090108320.md): Target · faulty · Aug 28, 2025 · N897UA · Airbus A319132 · Door Warning System
  > AFT CARGO DOOR OPEN INDICATION AT 3000 FT, DURING CLIMBOUT. C/W CARGO LATCH AND INDICATION CHECK. BOTH INDICATE NORMAL. ITEM IS INTERMITTENT. PROX SENSORS AND TARGETS. AFT CARGO DOOR OPEN/CLOSE PROX SENSOR (32WV) REPLACED. OP CHECK GOOD. ADJUSTEMT WITHIN
- [SDR CALA2025040203444](https://openairdocs.org/sdr/CALA2025040203444.md): Battery · discharged · Mar 30, 2025 · N897UA · Airbus A319132 · Emergency Lighting
  > OPERATIONAL CHECK OF CABIN EMERGENCY LIGHTS {A3NB-33-3-6012} - FWD BATTERY L FAIL TEST REPLECED FW EMERGENCY LIGHT BATTERY. REF: AMM 33-51-38. OPS CHECK GOOD.
- [SDR CALA2025031902940](https://openairdocs.org/sdr/CALA2025031902940.md): Slide · not reported · Mar 16, 2025 · N897UA · Airbus A319132 · Escape Slide
  > AFT DOOR ESCAPE SLIDE/RAFT REMOVE {A3NB-25-3-0023} - REMOVED R2 DOOR SLIDE IAW AMM 25-62-44-000-804-A. NEW SLIDE BAD FROM STOCK. P/N NIS @ EWR. STILL REQUIRES INSTALL. REMOVED AND REPLACED R2 DOOR PER AMM TASK 25-62-44-400-803-A SEE LOG PAGE FOR ROTABE PARTS 4
- [SDR CALA2025021902376](https://openairdocs.org/sdr/CALA2025021902376.md): Bottle · low pressure · Feb 15, 2025 · N897UA · Airbus A319132 · Escape Slide
  > DOOR 2L SLIDE PRESSURE GAUGE SHOWING IN YELLOW BAND. SERVICED L2 ASSIST BOTTLE PER AAM 12-14-00, NOW AT CORRECT PRESSURE
- [SDR CALA2024122301628](https://openairdocs.org/sdr/CALA2024122301628.md): Slat System · faulted · Dec 20, 2024 · N897UA · Airbus A319132 · Leading Edge Slat Control System
  > F/CTL SLATS LOCKED FOLLOWED TSM 27-81-00 LHAPPU AND RH APPU SYNCHRO ANGLES ARE WITHIN LIMITS. PERFORMED A RESET OF WING TIP BRAKES PER AMM 27-80-00. PERFORMED VISUAL INSPECTION OF SLAT TRANSMISSION ASSEMBLY AND MULTIPLE OPS TEST OF SLAT/FLAP SYSTEM PER AMM 2
- [SDR CALA2024112201246](https://openairdocs.org/sdr/CALA2024112201246.md): Battery Pack · no test · Nov 21, 2024 · N897UA · Airbus A319132 · Emergency Lighting
  > OPERATIONAL CHECK OF CABIN EMERGENCY LIGHTS {A3NB-33-3-6012} - LEFT EPSU BATTERY FAULT RPLD BATTERY IAW MM33-51-38, CIDS TEST PASS REFER LP 9929673 RIGHT EPSU BATTERY FAULT RPLD BATTERY IAW MM33-51-38, CIDS TEST PASS
- [SDR CALA2024110102768](https://openairdocs.org/sdr/CALA2024110102768.md): Control Servo · faulted · Oct 25, 2024 · N897UA · Airbus A319132 · Landing Gear System
  > WHEEL N/W STRG FAULT ECAM DISPLAYED UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. DO SYS REST AND OPS CHECK REF AMM 32-51-00-720-003-A MAC METER INITIATED FOR WITH VENDOR ID N079178 MAC RELATED WORK ORDER 00000000
- [SDR CALA2024102500932](https://openairdocs.org/sdr/CALA2024102500932.md): Control Servo · faulted · Oct 24, 2024 · N897UA · Airbus A319132 · Landing Gear Steering System
  > WHEEL N/W STRG FAULT ECAM DISPLAYED UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. DO SYS REST AND OPS CHECK REF AMM 32-51-00-720-003-A REMOVED AND REPLACED THE NOSE LANDING GEAR SERVO VALVE 6GC REF AMM 32-51-51P
- [SDR CALA2024071502042](https://openairdocs.org/sdr/CALA2024071502042.md): Rib · damaged · Jul 13, 2024 · N897UA · Airbus A319132 · Vertical Stabilizer, Spar/Rib
  > (A3NB-55-3-6022) NO DOT-VERTICAL STAB HINGE ARM TO RUDDER HINGE ARM FITTING 2 EA ATACHMENT HOLES ELONGATED AS MARKED.() REMOVED AND REPLACED BR 1 HINGE ARM AND 01 EA HINGE FITTING AT V ERTICAL STABILIZER I.A.W SRM 55-36-42-300-003 AND SRM 51-72-00/0 01. W/C:94
- [SDR CALA2024071502041](https://openairdocs.org/sdr/CALA2024071502041.md): Crossbeam · gouged · Jul 12, 2024 · N897UA · Airbus A319132 · Fuselage Main, Structure
  > CABIN FLOOR CROSSBEAMS AT FR 65 & 67 GOUGED DURING HMV3 AT BFM AS NOTED ON N/R'S 94470 & 94471. EA319-5341-13-A3610 WITH NO DEVIATIONS. INTERIM REPAIR AT FR 67 ACCOMPLISH INSPECTION REQUIREMENT PER PART 2 OF THE LATEST REQUIRES DIP PER PART 1.3 AS FOLLOWS: AT
- [SDR CALA2024070201953](https://openairdocs.org/sdr/CALA2024070201953.md): Frame · cracked · Jun 19, 2024 · N897UA · Airbus A319132 · Fuselage Main, Frame
  > CRACK INDICATION NOTED AT RH FR20 DOOR STOP FITTING #1, HOLE #3 WHILE ACCOMP''G INSP IAW EA5311-02164 (B), AT BFM HMV ON N/R 93794. 1.6 AS FOLLOWS: RH FR20 DOOR STOP FITTING #1, HOLE #3 WAS REP''D ER PART 2 OF LATEST REVISION OF ECRA5311-03231 ON/BEFORE ACFT R
- [SDR CALA2024061901867](https://openairdocs.org/sdr/CALA2024061901867.md): Fitting · cracked · Jun 18, 2024 · N897UA · Airbus A319132 · Fuselage Main, Structure
  > (SUPPORT TASK) DURING ROTO TEST AT LH FR16 DOOR STOP 7 LOWER INB OARD HOLE FOUND CRAKCED. "REPAIR BEFORE NEXT FLIGHT" W/C:93882 REPAIRED IAW EC/RA 5311-03221. W/C:93882 ALL REQUIRED INSPECTIONS COMPLIED ON WORKCARD # 93882
- [SDR CALA2024061901866](https://openairdocs.org/sdr/CALA2024061901866.md): Door Frame · cracked · Jun 15, 2024 · N897UA · Airbus A319132 · Fuselage Main, Structure
  > DURING INSP IAW EA5311-02164 (B), LT FR16 DOOR STOP FITTING #7 HOLE #1 & HOLE #3 FOUND CRACKED, ALSO LT FR20 DOOR STOP FITTING #1, HOLE #3 FOUND CRACKED. NOTED ON VTMAE N/RS 93881, 93882 & 93791. H 1.7. HOLES 1 & 3 WERE REPAIRED. ACCOMP INTERIM REPAIR IAW
- [SDR CALA2024070101938](https://openairdocs.org/sdr/CALA2024070101938.md): Stringer · corroded · Jun 13, 2024 · N897UA · Airbus A319132 · Fuselage Main, Longeron/Stringer
  > (A3NB-05-3-6029) FR 64-66 STRINGER 31 RH (ONE BAY FWD OF OUT FLO W VALVE FOUND CORRODED. W/C:94579 REMOVED AND REPLACED STRINGER 31 R/H BETWEEN FRAME 64-66 IAW SRM 51-42-11. W/C:94579 EMP:V941985 STA:STENGBFM
- [SDR CALA2024061301793](https://openairdocs.org/sdr/CALA2024061301793.md): Fitting · damaged · Jun 6, 2024 · N897UA · Airbus A319132 · Fuselage Main, Structure
  > LH FR4 OF WINDSHIELD SIDE POST ON AFT UPPER ATT AHCEMENT VISUAL DAMAGE (GOUGE) NOTED. W/C:94114 REMOVED AND REPLACED UPPER FITTING L/H FRAME 4 OF WINDSHIELD SIDE IAW FINAL INSTRUCTION OF EA#319-5311-13-A3598, SRM 51-42-11 AND PRODUCTION DRAWING R53111007. W/C:
- [SDR CALA2024062001875](https://openairdocs.org/sdr/CALA2024062001875.md): Seat Track · corroded · Apr 29, 2024 · N897UA · Airbus A319132 · Fuselage, Seat/Cargo Attach Fittings
  > (A3NB-53-4-6179)- MAIN CABIN R/H O/B SEAT TRACK BETWEEN FR 55-56 HAS CORROSION DOT 43-160. W/C:94483 REPAIRED SEAT TRACK R/H I/B BETWEEN FR 47 TO FR 57 IAW SRM 53-41 -15-300-003. W/C:944483 EMP:V936696 STA:STENGBFM
- [SDR CALA2024060301681](https://openairdocs.org/sdr/CALA2024060301681.md): Seat Track · corroded · Apr 29, 2024 · N897UA · Airbus A319132 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN L/H I/B SEAT TRACK BETWEEN FR 55-56 HAS CORROSION. REPAIRED SEAT TRACK VIA SPLICE REPAIR FROM FR 47 TO 56 IAW 53-41 -15-300-003 CAT A REPAIR. W/C:94489 ALL INSPECTIONS ACCOMPLISHED ON NRC 94489 AT BFM.
- [SDR CALA2024053001643](https://openairdocs.org/sdr/CALA2024053001643.md): Floorbeam · corroded · Apr 29, 2024 · N897UA · Airbus A319132 · Fuselage Main, Floor Beam
  > (SUPOORT TASK) FWD WET AREA FLOOR SUPPORT BEAM AT Y1292 FR 16 FOUND CORRODED AT HARD POINT. W/C:94421 REMOVED CORROSION ON FLOOR SUPPORT BEAM IAW 51-74-00, OUT OF LIM ITS IAW 53-11-14-283-007 L:2,628 W:1,651 D:0,049 T91554 REMOVED AND REPLACED SUPPORT BEAM IAW
- [SDR CALA2024052001529](https://openairdocs.org/sdr/CALA2024052001529.md): Seat Track · worn · Apr 29, 2024 · N897UA · Airbus A319132 · Fuselage, Seat/Cargo Attach Fittings
  > (A3NB-53-4-6179)- MAIN CABIN L/H O/B SEAT TRACK BETWEEN FR 43-44 HAS WEAR MARK DOT 43-170. W/C:94492 REMOVED AND REPLACED MAIN CABIN L/H O/B SEAT TRACK BETWEEN FR 43 -44 IAW SRM 51-42-11.
- [SDR CALA2024052001528](https://openairdocs.org/sdr/CALA2024052001528.md): Seat Track · corroded · Apr 29, 2024 · N897UA · Airbus A319132 · Fuselage, Seat/Cargo Attach Fittings
  > (A3NB-53-4-6179) - MAIN CABIN L/H O/B SEAT TRACK BETWEEN FR 40-4 1 HAS CORRSOION DOT 43-171. W/C:94495 REMOVED AND REPLACED MAINC ABIN L/H O/B SEAT TRACK BETWEEN FR 40 -41 IAW SRM 51-42-11.
- [SDR CALA2024061901868](https://openairdocs.org/sdr/CALA2024061901868.md): Door Sill · corroded · Apr 22, 2024 · N897UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > (A3NB-53-3-6222) DOT 95-111 - L2 PAX DOOR SILL SHOWS CORROSION. W/C:94252. REMOVED AND REPLACED DOOR SILL L2 LEFT SIDE IAW SRM 51-42-11/001 AND DRAWING D53480505. W/C:94252
- [SDR CALA2024070201954](https://openairdocs.org/sdr/CALA2024070201954.md): Floorbeam · damaged · Apr 20, 2024 · N897UA · Airbus A319132 · Fuselage Main, Floor Beam
  > AFT PAX CABIN FLOOR BEAM -Y765 FR66 HAS TOOL MARKS AS MARKED. () REMOVED FLOOR BEAM IAW SRM 51-42-11 RECIEVED NEW PART P/N D53472 EMP:V940839 STA:STENGBFM 23200600, BATCH# 0002836064 INSTALLED NEW FLOOR BEAM P/N D534722 3200600, IAW SRM 51-72-11-911-001 T =967
- [SDR CALA2024053001645](https://openairdocs.org/sdr/CALA2024053001645.md): Shear Plate · corroded · Apr 20, 2024 · N897UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > AFT WET AREA FR69 - FR70, L/H SHEAR PLATE SHOWS CORROSION. () REMOVED SHEAR PLATE AND SUPPORT FRAME IAW SRM 51-42-11, RECIEVED STA:STENGBFM NEW SHEAR PLATE P/N D5347112420200 SUPPORT FRAME P/N: D53471123 20200, LOCATED AND DRILL HOLE IAW SRM 51-44-11/001, INST
- [SDR CALA2024053001644](https://openairdocs.org/sdr/CALA2024053001644.md): Shear Plate · corroded · Apr 20, 2024 · N897UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > AFT WET AREA FR69 - FR70, R/H SHEAR PLATE SHOWS CORROSION. () REMOVED SHEAR PLATE AND SUPPORT FRAME IAW SRM 51-42-11 RECIEVED 9 STA:STENGBFM NEW SHEAR PLATE D5347112420300 SUPPORT FRAME D5347112320300, LOC ATED AND DRILL HOLE IAW SRM 51-44-11/001. INSTALLED NE
- [SDR CALA2024050101292](https://openairdocs.org/sdr/CALA2024050101292.md): Seat Track · corroded · Apr 20, 2024 · N897UA · Airbus A319132 · Fuselage, Seat/Cargo Attach Fittings
  > AFT PAX CABIN FLOOR BEAM Y765 / FR68 SURFACE SHOWS CORROSION. () REMOVED AND REPLACED FLOOR BEAM Y265 BETWEEN FR 66 TO 70 IAW SRM 51-42-11. W/C:94256 EMP:V941985 STA:STENGBFM
- [SDR CALA2024061901872](https://openairdocs.org/sdr/CALA2024061901872.md): Door Frame · cracked · Apr 12, 2024 · N897UA · Airbus A319132 · Fuselage Main, Structure
  > (AD 2022-02-11) DURING ROTO INSPECTION OF RH FR16 DOOR STOP #7. CRACK INDICATION NOTED IN UPPER I/B HOLE AT FRAME AND INTERCOSTA L LAYERS. REPAIR BEFORE NEXT FLIGHT.() REPAIRED PER EC/RA 5311-03231 PART 1. W/C:93792 ALL MANDATORY INSPECTIONS WERE COMPLETED ON
- [SDR CALA2024061901870](https://openairdocs.org/sdr/CALA2024061901870.md): Door Frame · cracked · Apr 12, 2024 · N897UA · Airbus A319132 · Fuselage Main, Structure
  > (AD 2022-02-11) DURING ROTO INSPECTION OF RH FR16 DOOR STOP #7 C RACK INDICATION NOTED IN LOWER HOLE AT FRAME AND INTERCOSTAL LAY ERS. REPAIR BEFORE NEXT FLIGHT.() REPAIRED PER EC/RA 5311-03231. W/C:93793 STA:STENGBF M ALL REQUIRED INSPECTIONS COMPLETED AT STE
- [SDR CALA2023121803658](https://openairdocs.org/sdr/CALA2023121803658.md): Outflow Valve · malfunctioned · Dec 17, 2023 · N897UA · Airbus A319132 · Pressure Regulator/Outflow Valve
  > CABIN WOULD NOT PRESSURIZE AT FL010 WHEN ALARM WENT OFF DURING TAKE OFF. CA SWITCHED FROM CONTROLLER 1 TO 2. STARTED WORKING ON WAY TO LAND. FLAGGED SDR PFR SHOWS SDAC2:NO CPC1 ANALOG SIGNAL. ADDED PHOTO OF PFR. REPLACED OUTFLOW VALVE IN REFERENCE TO AMM 21-31
- [SDR CALA2022123003522](https://openairdocs.org/sdr/CALA2022123003522.md): Computer · faulted · Dec 30, 2022 · N897UA · Airbus A319132 · Flight Environment Data
  > GATE RETURN, NAV FO AOA FAULT. AT ROTATION ECAM FLT CNTRL ALT LAW PROTECTIONS LOST. NO INDICATION TO WHY. STRONG CROSSWIND PRESENT. SYSTEM NORMAL DIRECT LAW TAKEOVER AT GEAR DOWN. AT ENG SHUT DOWN ECAM MSG NAV FO AOA FAULT. DURING ENTIRE FLIGHT AC HAD TEND
- [SDR CALA2022091602393](https://openairdocs.org/sdr/CALA2022091602393.md): Fuel Cap · missing · Sep 15, 2022 · N897UA · Airbus A300* · Aircraft Fuel System
  > THIS IS A SUPPLEMENTAL REPORT FOR THE SAME CONTROL NUMBER SUBMITTED ON 9/16/22. PDA 3 OPS REPORTS FUEL CAP LANYARD IS MISSING. REPLACED FUEL CAP AND LANYARD.
- [SDR CALA2022010500033](https://openairdocs.org/sdr/CALA2022010500033.md): Lamp · missing · Jan 5, 2022 · N897UA · Airbus A300* · Exterior Lighting
  > AIRCRAFT CAME IN MISSING LAMP FROM LANDING LIGHT ASSY, ITEM PLACED ON CDL.
- [SDR CALA2017122804653](https://openairdocs.org/sdr/CALA2017122804653.md): Seal · corroded · Dec 28, 2017 · N897UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > R2 DOOR SILL FWD SHAPE SEAL HAS SURFACE CORROSION. REMOVED AND REPLACED THE DOOR SHAPE SEAL AT FRAME 66 IAW SRM 51-42-11-001.
- [SDR CALA2017121604475](https://openairdocs.org/sdr/CALA2017121604475.md): None · none · Dec 16, 2017 · N897UA · Airbus A319132 · Standard Practices/Structures
  > SUPPORT TASK-EXISTING DOUBLER REPAIR AT FR60 STR 41L-STR 42L REQUIRES EVALUATION & ARCHIVE. REMOVED EXISTING REPAIR AT FR 60 STRINGER 41L-42L. FABRICATED NEW DOUBLER MADE OF CLAD 2024-T3-.080" PER SRM 53-41-11-300-037 PARA 2 (A) FIGURE 20129. THIS REPAIR REQUI
- [SDR CALA2017121504461](https://openairdocs.org/sdr/CALA2017121504461.md): Seal · corroded · Dec 15, 2017 · N897UA · Airbus A319132 · Fuselage Main, Structure
  > AFT WET AREA L2 DOOR SILL MID SECTION SHAPE SEAL HAS CORROSION. L2 DOOR SILL MID SECTION FITTING FOUND TO HAVE 100% MATERIAL LOSS. REMOVED OLD DOOR SILL MID SECTION FITTING. REPLACED WITH NEW DOOR SILL MID SECTION FITTING PN 5348004820203 IAW A319 SRM 51-7 2-
- [SDR CALA2017121504460](https://openairdocs.org/sdr/CALA2017121504460.md): Stringer · corroded · Dec 15, 2017 · N897UA · Airbus A319132 · Fuselage Main, Longeron/Stringer
  > BULK CARGO COMPARTMENT STRINGER 43L FR 66-68 HAS EVIDENCE OF CORROSION. REPAIRED STR 43L IAW A319 SRM 53-00-13-300-002 PARA 2
- [SDR CALA2017121504459](https://openairdocs.org/sdr/CALA2017121504459.md): Door Sill · corroded · Dec 15, 2017 · N897UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > L2 DOOR SILL FWD SHAPE SEAL HAS SURFACE CORROSION. L2 DOOR SILL CORNER SHAPE FITTING FOUND TO HAVE 100% MATERIAL LOSS. REMOVED & REPLACED OLD DOOR CORNER SHAPE FITTING WITH NEW DOOR CORNER SHAPE FITTING PN D5398004220402 IAW A319 SRM 51-72-11 REV 119
- [SDR CALA2017121504458](https://openairdocs.org/sdr/CALA2017121504458.md): Stringer · corroded · Dec 15, 2017 · N897UA · Airbus A319132 · Fuselage Main, Longeron/Stringer
  > BULK CARGO COMPARTMENT STRINGER 44L FR 66-68 HAS EVIDENCE OF CORROSION. REPAIRED STR 44 AT FR66-FR68 IAW A319 SRM 53-00-13-300-002 PARA 2
- [SDR CALA2017121504457](https://openairdocs.org/sdr/CALA2017121504457.md): Fitting · corroded · Dec 15, 2017 · N897UA · Airbus A319132 · Fuselage Main, Attach Fittings
  > AFT WET AREA R2 DOOR SILL AFT CORNER BELOW GIRT BAR FITTING HAS CORROSION. REMOVED CORROSION R2 DOOR SILL AFT CORNER WITH.035 MAT. LOSS FR OM ORIGINAL.177, FOUND TO BE BEHOND LIMITS IAW A319 SRM 53-41-1 4-283-002 FIG 10101. REMOVED & REPLACED R2 DOOR SILL I
- [SDR CALA2017121304424](https://openairdocs.org/sdr/CALA2017121304424.md): Bulkhead · cracked · Dec 12, 2017 · N897UA · Airbus A319132 · Fuselage Main, Bulkhead
  > SUPPORT TASK: AD 2014-24-07: UPON ROTO-PROBE INSPECTION OF FR43 FOUND HOLES 9 & 10 TO HAVE CRACK INDICATIONS. PRESSURE PLATE P/N D5337056920700 REMOVAL & REPLACEMENT ACCOMPLI SHED ON EA 5331-01704 OP 007.
- [SDR CALA2017121304423](https://openairdocs.org/sdr/CALA2017121304423.md): Bulkhead · cracked · Dec 12, 2017 · N897UA · Airbus A319132 · Fuselage Main, Bulkhead
  > SUPPORT TASK: AD 2014-24-07: UPON RE-IN SPECTION (ROTO SCAN) OF HOLE 9 AT FR43 FOUND CRACK INDICATION TO BE IN PRESSURE PLATE ONLY. REMOVED & REPLACED PRESSURE PLATE ON L/H SIDE IAW EA 5331-01704 OP 006

## 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 = 'N897UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N897UA/reports

---
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