# Service difficulty reports: IAE V2522-A5

A list on [IAE V2522-A5](https://openairdocs.org/engine/iae-v2522-a5.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 70 · 3,460 reports

- [SDR CALA2026102220518](https://openairdocs.org/sdr/CALA2026102220518.md): Elec Connector · fod · Oct 22, 2026 · N804UA · Airbus A319131 · Landing Gear System Wiring
  > BRAKES AUTO BRK FAULT ECAM ON FINAL APPROACH, DID CHECKLIST, CYCLED LANDING GEAR, NORMAL LANDING AND BRAKES POST FLT FAULTING BRK SELECTOR VALVE (23GG) ON BSCU 2. RAN NORMAL BRAKING AND LRU WIRING AND BSCU TEST BOTH FAULTING BRK SELECTOR VALVE (23GG). NO FAULT
- [SDR CALA2026102220526](https://openairdocs.org/sdr/CALA2026102220526.md): Floor Support · cracked · Oct 20, 2026 · N836UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > FWD CARGO, FRMS 28 - 34, STR 35R. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11/001 2E, SRM 51-44-11/001, SRM 51-46-11/00 1, & SRM 51-75-12-911-002.
- [SDR CALA2026102120482](https://openairdocs.org/sdr/CALA2026102120482.md): Unknown · odor · Oct 19, 2026 · N831UA · Airbus A319131 · Air Distribution System
  > FUMES THROUGHOUT ACFT AFTER SHUTDOWN OF NR 2 ENGINE AND OPENING APU BLEED. RAN APU & BLEED TO VERIFY ODOR IN CABIN, ACCOMPLISHED INSPECTION IAW AMM 05-50-00-810-831-A. OPS APU FOR EXTENDED PERIOD & PACKS USING APU BLEED. NO ODORS NOTED DURING OPS.
- [SDR CALA2026102120493](https://openairdocs.org/sdr/CALA2026102120493.md): Flashlight · no discrepancy · Oct 17, 2026 · N831UA · Airbus A319131 · Emergency Equipment
  > AFT FLASHLIGHT NEAR FLIGHT ATTENDANT JUMPSEAT BATTERY FLASHING RED INOP STICKER INSTALLED ON THE AFFECTED FLASHLIGHT BY THE CAPTAIN. AFT OTBD FLASHLIGHT WORKING NORMAL. NO RED LIGHT, TESTING FUNCTION PRODUCES GREEN LIGHT CONSISTENT WITH OTHER FLASHLIGHTS. INO
- [SDR CALA2026101920451](https://openairdocs.org/sdr/CALA2026101920451.md): Hydraulic Line · leaking · Oct 15, 2026 · N802UA · Airbus A319131 · Hydraulic System, Main
  > GREEN HYD SYS LOW PRESSURE. ECAM RUN MANUAL GEAR EXTENSION. FOUND HYD LINE LEAKING IN LEFT WING BETWEEN RIB 1 AND RIB 2. REMOVED LINE #30 REF IPC 29-11-05-02. REPLACED LEAKING LINE WITH SERVICABLE ONE REF LINE #30 REF IPC 29-11-05-02. LEAK CHECKS GOOD, RESET
- [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 CALA2026101320358](https://openairdocs.org/sdr/CALA2026101320358.md): Power Supply · faulted · Oct 12, 2026 · N817UA · Airbus A319131 · Emergency Lighting
  > TEST OF THE EMERGENCY LIGHTS FAILS WITH EPSU INT LOAD EMER R, EPSU BATTERY AFT L AND EPSU UNIT EMER L MESSAGES. R&R RIGHT OVER WING EPSU REF AMM 33-51-400-001-A. R&R AFT BATTERY OF EPSU REF AMM 33-51-38-000-002-A. OPS CHECK GOOD. NO FAULTS NOTED AT THIS TIME.
- [SDR CALA2026101320357](https://openairdocs.org/sdr/CALA2026101320357.md): Light · inoperative · Oct 11, 2026 · N811UA · Airbus A319131 · Emergency Lighting
  > AISLE SEAT 8C EMERGENCY LIGHT INOP. REMOVED AND REPLACED PATHWAY ILLUMINATION LIGHT ON SEAT 8C IN REFERENCE TO AMM 33-51-19. OPS CHECK GOOD. PARTS USED: BR9644-21,QTY:1
- [SDR CALA2026101320315](https://openairdocs.org/sdr/CALA2026101320315.md): Floor Support · corroded · Oct 10, 2026 · N836UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT FLOORBOARD PROFILE AT FR 58-59 STR 38L, FLOORBOARD RISER/RAMP CORRODED. REMOVED AND REPLACED AFT CARGO FLOORBOARD RISER AT FR 58-59 STR 38L IAW SRM 51-42-11 AND SRM 51-72-11-911-001.
- [SDR CALA2026100920246](https://openairdocs.org/sdr/CALA2026100920246.md): Frame · cracked · Oct 8, 2026 · N824UA · Airbus A319131 · Fuselage Main, Frame
  > RIGHT FRAME 16 DOUBLE JOGGLE AREA HOLE 5, HAS A CRACK INDICATION IN CORNER DOUBLER LAYER AT 6 OCLOCK DIRECTION 100%. ACCOMPLISHED A REPAIR IAW REO L26059, REV IR, AND ECRA 5311-03084, REV A.
- [SDR CALA2026100820218](https://openairdocs.org/sdr/CALA2026100820218.md): Access Panel · damaged · Oct 7, 2026 · N848UA · Airbus A319131 · Wing, Plate/Skin
  > DURING REMOVAL OF ACCESS PANEL 540KB, ACFT SKIN WAS DAMAGED. EXCEEDED LIMITS OF SRM 57-21-11-300-002, INTERIM REPAIR PERFORMED TO FUEL ACCESS PANEL 540KB IAW PART 1 OF ECRA 5721-01445. ACCOMPLISH PERMINATE REPAIR AT LT WING BOTTOM FUEL ACCESS PANEL 540KB HO
- [SDR CALA2026100720173](https://openairdocs.org/sdr/CALA2026100720173.md): Seat Track · corroded · Oct 5, 2026 · N836UA · Airbus A319131 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION LOCATED AT SEAT TRACK Y-1292 AND FRAME 20. REMOVED SEAT TRACK Y-1292 FR12-FR24 IAW A319 SRM 51-42-11/001 RE V 159 PAR 2.F, REPLACED SEAT TRACK Y-1292 FR12-FR24 IAW A319 SRM 51-42-11/001 REV.159 PAR. 2.F.
- [SDR CALA2026100720181](https://openairdocs.org/sdr/CALA2026100720181.md): Seat Track · corroded · Oct 5, 2026 · N836UA · Airbus A319131 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK Y-765 AND FRAME 20 2 AEREAS. REMOVED AND REPLACED SEAT TRACK 765 IAW A319 SRM 51-42-11 FROM F R12-FR24.
- [SDR CALA2026100520102](https://openairdocs.org/sdr/CALA2026100520102.md): Fuel Cap · missing · Oct 3, 2026 · N823UA · Airbus A319131 · Fuel Storage
  > MISSING FUEL CAP UPON ARRIVAL. INSTALLED A FUEL CAP.
- [SDR CALA2026100620130](https://openairdocs.org/sdr/CALA2026100620130.md): Floorbeam · corroded · Oct 3, 2026 · N836UA · Airbus A319131 · Fuselage Main, Floor Beam
  > AFT WET AREA, LT FLOOR BEAM Y160.5, BARREL NUT CORRODED IN LAV MOUNT FITTING, JUST AFT OF FR 68. REMOVED AND REPLACED L/H FLOOR BEAM Y160.5 FR68-70 IAW A319 SRM 51-72-11-911-001
- [SDR CALA2026100620132](https://openairdocs.org/sdr/CALA2026100620132.md): Window Frame · cracked · Oct 3, 2026 · N836UA · Airbus A319131 · Fuselage Main, Structure
  > RIGHT WINDSHIELD FRAME CONTINUITY FITTING AREA ROTO TEST INSPECTIO N FOUND CRACK INDICATION IN MOST I/B HOLE GEN BY V929087 ON AAR LCQ NR 9298821/26821 UP DATED EFSR REPAIRED R/H WINDSHIELD FRAME MOSL I/B FASTENER HOLE IAW A319 EC RA NO.5311-03421 OVERSIZE AND
- [SDR CALA2026100520071](https://openairdocs.org/sdr/CALA2026100520071.md): Light · disconnected · Oct 2, 2026 · N848UA · Airbus A319131 · Light System Wiring
  > EMERGENCY LIGHTS AT SEATS 27C AND 28C WILL NOT ILLUMINATE. FOUND LIGHT ASSEMBLIES AT SEATS 27C AND 28C TO BE DISCONNECTED. CONNECTED LIGHTING ASSEMBLIES AND PERFORMED OPS CHECK IAW AMM 33-51-00. OPS CHKD GOOD.
- [SDR CALA2026092920000](https://openairdocs.org/sdr/CALA2026092920000.md): Floor Support · corroded · Sep 29, 2026 · N836UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY FLOOR SUPPORT, FR 52-56, STR38L HAD MULTIPLE SPOTS OF CORROSION. REMOVED AND REPLACED AFT CARGO COMPARTMENT FLOOR SUPPORT IAW SRM 51-41-4.
- [SDR CALA2026092920004](https://openairdocs.org/sdr/CALA2026092920004.md): Floor Support · corroded · Sep 29, 2026 · N836UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT FLOOR BOARD PROFILE AT FR 56-58 STR38L HAS MULTIPLE SPOTS OF CORROSION. REMOVED AND REPLACED AFT CARGO COMPARTMENT FLOOR BOARD PROFILE A T FR56-58 STR 38L IAW A319 SRM 51-44-11.
- [SDR CALA2026101320340](https://openairdocs.org/sdr/CALA2026101320340.md): Feeder Cable · damaged · Sep 27, 2026 · N827UA · Airbus A319131 · Electrical Power System Wiring
  > DURING ALI VISIT, FOUND RT PYLON IDG FEEDER CABLE WIRE 2422-4519 INSULATION DAMAGED UNDER PANEL 521BT BETWEEN RIB 5A & PS 6480/RIB09 STA MLB. PERFORMED DAMAGE ASSESSMENT OF RT PYLON WIRE 2422-4519 IAW ESPM 20-53-21-02. REPAIRED WIRE WITH A GRADE 3 TEMP REPAIR
- [SDR CALA2026092819919](https://openairdocs.org/sdr/CALA2026092819919.md): Skin · damaged · Sep 25, 2026 · N836UA · Airbus A319131 · Elevator, Plate/Skin
  > LEFT TOP & BOTTOM SKIN PANEL FOUND LIQUID ENGRESS INDICATION AT 160" FROM INBD EDGE, AND 9 1/2" FROM T/E. DEFECT IS 2 INCHES IN SIZE. REPAIRED THE LT ELEVATOR TOP SKIN 160IN FROM INBD EDGE 9.5IN FROM T/E 2 INCHES IN DIA IAW SRM 55-21-11-300-005.
- [SDR CALA2026092819921](https://openairdocs.org/sdr/CALA2026092819921.md): Skin · damaged · Sep 25, 2026 · N836UA · Airbus A319131 · Elevator, Plate/Skin
  > LEFT TOP SKIN PANEL FOUND LIQUID ENGRESS INDICATION AT 146 INCHES FROM INBD EDGE AND 12 1/2 INCHES FROM T/E. DEFECT IS 1 3/4 INCH IN SIZE. REPAIRED THE LT ELEVATOR TOP SKIN IAW SRM 55-21-11-300-005. CATEGORY A REPAIR.
- [SDR CALA2026092519834](https://openairdocs.org/sdr/CALA2026092519834.md): Panel · corroded · Sep 24, 2026 · N836UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT SLOPING PANEL PROFILE AT FR 54-56, STR 35R HAD MULTIPLE SPOTS OF CORROSION. REMOVED AND REPLACED AFT CARGO SLOPING PANEL PROFILE IAW SRM 51-42-11.
- [SDR CALA2026092519836](https://openairdocs.org/sdr/CALA2026092519836.md): Floor Support · corroded · Sep 24, 2026 · N836UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY FLOOR SUPPORT AT FR 59-63, STR 38L HAS MULTIPLE SPOTS OF CORROSION. REMOVED AND REPLACED THE AFT CARGO PROFILE PANEL IAW SRM 51-42-11.
- [SDR CALA2026092519838](https://openairdocs.org/sdr/CALA2026092519838.md): Floorbeam · damaged · Sep 24, 2026 · N836UA · Airbus A319131 · Fuselage Main, Floor Beam
  > FWD CARGO FLOORBEAM, FR28, STR 38R-38L HAD MULTIPLE ELONGATED HOLES. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-42-11-001A,
- [SDR CALA2026092819854](https://openairdocs.org/sdr/CALA2026092819854.md): Oil System · low · Sep 24, 2026 · N814UA · Airbus A319131 · Turbine Engine Oil System
  > ENG 1 LOW OIL, AFTER ROTATIONIND 4.5 QT AFTER LEVEL OFF 6-8 QT ENGINE 1 FAN COWLS AND THRUST REVERSERS OPENED TO PERFORM VISUAL INSP OF ENGINE. NO LEAKS NOTED. SERVICED ENGINE WITH 9 QUARTS OF OIL AND PERFORMED DRY MOTOR OF ENGINE 1 IAW AMM TASK 71-00-00-710-0
- [SDR CALA2026092519805](https://openairdocs.org/sdr/CALA2026092519805.md): Fitting · corroded · Sep 23, 2026 · N836UA · Airbus A319131 · Fuselage Main, Structure
  > L2 DOOR CUTOUT, AFT CORNER FITTING CORRODED. REMOVED AFT CORNER ON L2 DOOR IAW SRM 51-42-11/001, REV 159, PAR 2.G, 2.F. REPLACED THE AFT CORNER ON L2 DOOR IAW SRM 51-42-1 1/001, REV 159. PARA 2.E,2.F.
- [SDR CALA2026092819868](https://openairdocs.org/sdr/CALA2026092819868.md): Profile · corroded · Sep 23, 2026 · N836UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > FWD PIT PROFILE AT FR 27, S38L WAS CORRODED. REMOVED AND REPLACED FWD PIT PROFILE IAW SRM 5 1-42-11.
- [SDR CALA2026092419768](https://openairdocs.org/sdr/CALA2026092419768.md): Fitting · corroded · Sep 21, 2026 · N836UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > FRAME 68 HAS A DRILLED OUT FASTENER WITH CORROSION AROUND IT AFT CABIN. REMOVED AND REPLACED FITTING AT AFT CABIN FLOOR IAW SRM 51-42-11.
- [SDR CALA2026092519801](https://openairdocs.org/sdr/CALA2026092519801.md): Panel · missing · Sep 21, 2026 · N818UA · Airbus A319131 · Nacelle/Pylon, Main Frame
  > FOUND NR 1 PYLON SECTION PANEL MISSING, REF IPC 54-57-22-07A, ITEM 90, DETERMINED TO BE CATEGORY 2 50.75 SQ-IN R & R THE PYLON TO NACELLE PROFILE PANEL INBD IAW AMM 54-57-22.
- [SDR CALA2026092219660](https://openairdocs.org/sdr/CALA2026092219660.md): Panel · cracked · Sep 19, 2026 · N836UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > FWD CARGO LT BOTTOM SLANT FLOOR PROFILE HAD MULTIPLE CRACKS AROUND FASTENER HOLES AT FR 28 +10 IAW AAR LCQ N/R 9298507/26507. REMOVED AND REPLACED FWD CARGO PROFILE PANEL IAW SRM 51-42- 11.
- [SDR CALA2026092219662](https://openairdocs.org/sdr/CALA2026092219662.md): Seal · cracked · Sep 19, 2026 · N836UA · Airbus A319131 · Nacelle/Pylon, Main Frame
  > RIGHT PYLON FWD INBD BLADE SEAL CRACKED. REMOVED AND REPLACED BLADE SEAL AT RT PYLON FWD INBD IAW SRM 51-42-11.
- [SDR CALA2026092219664](https://openairdocs.org/sdr/CALA2026092219664.md): Panel · cracked · Sep 19, 2026 · N836UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > FWD CARGO RT BOTTOM SLANT TO FLOOR PROFILE STR 38 HAD A CRACK AT FR 28 +1. REMOVED AND REPLACED PROFILE PANEL ON FWD CARGO BAY IAW SRM 51-42-11-001.
- [SDR CALA2026092219666](https://openairdocs.org/sdr/CALA2026092219666.md): Floorboard · corroded · Sep 19, 2026 · N836UA · Airbus A319131 · Fuselage Floor Panel
  > AFT CARGO BAY CENTER FLOORBOARD AT FR 51 HAD MULTIPLE SPOTS OF CORROSION. REMOVED AND REPLACED AFT CARGO PROFILE PANEL AT FR57 IAW SRM 51-42-11.
- [SDR CALA2026092219668](https://openairdocs.org/sdr/CALA2026092219668.md): Floorboard · corroded · Sep 19, 2026 · N836UA · Airbus A319131 · Fuselage Floor Panel
  > AFT CARGO COMPARTMENT FLOORBOARD AT FR 59 - 63, STR 38R HAD MULTIPLE SPOTS OF CORROSION. REMOVED AND REPLACED AFT CARGO FLOORBOARD IAW SRM 51-42-11.
- [SDR CALA2026092219670](https://openairdocs.org/sdr/CALA2026092219670.md): Floorboard · corroded · Sep 19, 2026 · N836UA · Airbus A319131 · Fuselage Floor Panel
  > AFT CARGO BAY, FLOORBOARD AT FR 51-52, STR 38R HAD MULTIPLE SPOTS OF CORROSION. REMOVED AND REPLACED THE FLOORBOARD IAW SRM 51-42-11.
- [SDR CALA2026092219672](https://openairdocs.org/sdr/CALA2026092219672.md): Floorboard · corroded · Sep 19, 2026 · N836UA · Airbus A319131 · Fuselage Floor Panel
  > AFT CARGO BAY FLOORBOARD AT FR 52-56, STR 38R HAD MULTIPLE SPOTS OF CORROSION. REMOVED AND REPLACED FLOORBOARD IAW SRM 51-42-11.
- [SDR CALA2026092119613](https://openairdocs.org/sdr/CALA2026092119613.md): Wire Harness · faulted · Sep 18, 2026 · N807UA · Airbus A319131 · Engine Fuel System Wiring
  > NORMAL START ON NUMBER 1 ENGINE. REJECTED TAKEOFF APPROX 60 KNOTS DUE TO NR 1 EGT READING 162 DEGREES. OTHERWISE NORMAL ENGINE INSTRUMENTS AND ACCELERATION NO SWERVING. ADDED FADEC 1B TEST RESUT PICTURE REF TSM 77-20-00-810-801-B, PERFORMED ENG 1 ECTRICAL CA
- [SDR CALA2026092119615](https://openairdocs.org/sdr/CALA2026092119615.md): Panel · corroded · Sep 18, 2026 · N836UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > FWD CARGO SLOPING PANEL VERTICAL PROFILE 10" FWD OF FR30, STR 38R CORRODED. REMOVED AND REPLACED FWD CARGO PROFILE PANEL AT FR 30, STR 38R IAW SRM 51-42-11.
- [SDR CALA2026092119617](https://openairdocs.org/sdr/CALA2026092119617.md): Support · corroded · Sep 18, 2026 · N836UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT WET AREA, LT FR 69 - 70, SHEAR PLATE SUPPORT CORRODED. REMOVED AND REPLACED SHEAR PLATE SUPPORT ON AFT WET AREA BTW FR 70 -FR 69 LT STR 23 IAW SRM 51-42-11.
- [SDR CALA2026092119626](https://openairdocs.org/sdr/CALA2026092119626.md): Frame · corroded · Sep 18, 2026 · N819UA · Airbus A319131 · Fuselage Main, Frame
  > AFT CARGO FR 59 HAD CORROSION AT FASTENER HOLES. PERFORMED PERMANENT A REPAIR AT FR 59 IAW EC/RA 5341-01583.
- [SDR CALA2026101220280](https://openairdocs.org/sdr/CALA2026101220280.md): Gusset · cracked · Sep 18, 2026 · N836UA · Airbus A319131 · Fuselage Main, Structure
  > FRAME 66, STRINGER 14R, GUSSET PLATE MIDDLE HOLE IS VISIBLY ELONGATED IN GUSSET PLATE LAYER. THE GUSSET PLATE WAS R & R IAW SRM 53-41-12-300-018, FIGURE 1.
- [SDR CALA2026091819548](https://openairdocs.org/sdr/CALA2026091819548.md): Door Frame · cracked · Sep 17, 2026 · N836UA · Airbus A319131 · Fuselage Main, Structure
  > RIGHT EMERGENCY EXIT, FWD LOAD TRANSMITTING PROFILE SHOWS SIGNS OF CRACKING. REMOVED & REPLACED THE FRAME SEGMENT IAW SRM 51-72-11-911-001, & SRM 51-42-11-001.
- [SDR CALA2026092219642](https://openairdocs.org/sdr/CALA2026092219642.md): Shear Plate · corroded · Sep 17, 2026 · N836UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT WET AREA, RT FR 69 - 70,SHEAR PLATE CORRODED. REMOVED AND REPLACED SHEAR PLATE IAW SRM 51-42-11/001 AND 5 1-72-11-911-002.
- [SDR CALA2026092219644](https://openairdocs.org/sdr/CALA2026092219644.md): Door Sill · corroded · Sep 17, 2026 · N836UA · Airbus A319131 · Fuselage Main, Structure
  > L2 DOOR SILL HAS CORROSION JUST INBD OF AFT GIRT BAR FITTING. EVALUATED & REPAIRED L-2 DOORSILL JUST INBD OF AFT GIRT BAR FITTING, REPAIR/EVAL FOUND TO BE CATEGORY A NO FURTHER ACTION REQUIRED IAW SRM 53-41-14-300-001, & 53-41-14-283-002.
- [SDR CALA2026101220271](https://openairdocs.org/sdr/CALA2026101220271.md): Gusset · cracked · Sep 17, 2026 · N836UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > FR 66, STR 16L GUSSET PLATE TOP HOLE HA S A REJECTABLE INDICATION. GUSSET PLATE REMOVED AND REPLACED IAW SRM 53-41-12-300-018, FIGURE 1. FLOWCHART SOLUTION 1. GVI & HFEC INSPECTION COMPLETED PER NTMS 51-90-00, 5110-08 AND 51-10-01. NO DAMAGE FOUND ON FRAME I
- [SDR CALA2026101220275](https://openairdocs.org/sdr/CALA2026101220275.md): Gusset · cracked · Sep 17, 2026 · N836UA · Airbus A319131 · Fuselage Main, Structure
  > FRAME 68, STRINGER 12R, GUSSET PLATE MIDDLE HOLE IS VISIBLY ELONGATED IN GUSSET PLATE LAYER. GUSSET PLATE R & R IAW SRM 53-41-12-300-018, FIGURE 1.
- [SDR CALA2026101220277](https://openairdocs.org/sdr/CALA2026101220277.md): Gusset · cracked · Sep 17, 2026 · N836UA · Airbus A319131 · Fuselage Main, Structure
  > FRAME 68, STRINGER 14L GUSSET PLATE 2ND HOLE FROM BOTTOM IS VISIBLY OUT OF ROUND. THE GUSSET PLATE WAS R & R IAW SRM 53-41-12-300-018, FIGURE 1.
- [SDR CALA2026091719510](https://openairdocs.org/sdr/CALA2026091719510.md): Fuel Cap · missing · Sep 13, 2026 · N846UA · Airbus A319131 · Fuel Storage
  > FUEL CAP MISSING, CAP FOUND MISSING UPON ARRIVAL. EWR WAS PREVIOUS STATION THEY DID NOT FIND THE CAP AT THIS TIME. INSTALLED A NEW FUEL CAP IAW AMM 28-25-41-400-005-A. REMOVED PLACARD.
- [SDR CALA2026091519458](https://openairdocs.org/sdr/CALA2026091519458.md): Fuel Cap · missing · Sep 10, 2026 · N823UA · Airbus A319131 · Fuel Storage
  > PDA 2 FUELER REPORTING FUEL CAP MISSING REPLACED MISSING FUEL CAP P/N 0727540 PER AMM 28-25-41-00 PARTS USED: 31-2825-9-0001,QTY:1 MFG PN ON - 0727540 MFG SN ON - C260145 M&E SN ON - 00145 M&E PN ON - 31-2825-9-0001 MFG SN OFF - UNABLE TO IDENT MFG PN OFF -

Next page: https://openairdocs.org/engine/iae-v2522-a5/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 engine_model_key = 'V2522A5'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/iae-v2522-a5/reports

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