# Service difficulty reports: N899UA

A list on [N899UA](https://openairdocs.org/aircraft/N899UA.md).

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

- [SDR CALA2026091819538](https://openairdocs.org/sdr/CALA2026091819538.md): Fire Bottle · discharged · Sep 16, 2026 · N899UA · Airbus A319132 · Fire Bottle, Fixed
  > TROUBLESHOOT LOUD NOISE FROM APU FIRE BOTTLE AREA. UPON INSPECTION, APU FIRE BOTTLE FOUND DISCHARGED.APU FIRE BOTTLE. REMOVED AND REPLACED IAW AMM 26-22-41-000-001-A AND MM 26-22-41-400-001-A.OPC GOOD IAW AMM 26-22-00-710-001-A.
- [SDR CALA2026092819929](https://openairdocs.org/sdr/CALA2026092819929.md): Skin · ground damage · Sep 13, 2026 · N899UA · Airbus A319132 · Fuselage Main, Plate/Skin
  > DENT BELOW FORWARD CARGO DOOR DUE TO BELT LOADER CONTACT. DENT EVALUATED PER SRM 53-21-11-283-020. DENT MEASURES 2.5" LONG AND 1" WIDE 1" FWD OF FR 27 BTWN STRINGERS 42-43R WITH A MAX DEPTH OF 0.015". DENT IS TYPE 1 & LOCATED IN ZONE 1, FIGURE 7 & AREA 1, F
- [SDR CALA2025111411208](https://openairdocs.org/sdr/CALA2025111411208.md): Controller · faulted · Nov 10, 2025 · N899UA · Airbus A319132 · Cabin Pressure Controller
  > CABIN PRES WARNING AT FL390. PILOTS STATED THEY SAW A FLUCTUATION OF 2500 FT BUT FELT NO PRESSURE IN EARS.CPC 2 TOOK OVER RIGHT AFTER CPC 1 FAIL. PERFORMED CPC1 OPS CHECK SEVERAL TIMES WITH NO FAILURES. IAW AMM TASK 21-31-34-400-001-A,
- [SDR CALA2025110911025](https://openairdocs.org/sdr/CALA2025110911025.md): Girt Bar · frayed · Nov 7, 2025 · N899UA · Airbus A319132 · Emergency Equipment
  > REMOVED L1 DOOR SLIDE ASSY PER AMM TASK 25-62-44-000-012-A FOR FURTHER TROUBLESHOOTING. CLEARANCE FOR INSTAL L1 SLIDE NEW 1L SLIDE P/N D30664-705 S/N A5775 GIRT BAR LACING IS FRAYING IN MULTIPLE AREAS. INSTALLED L1 DOOR SLIDE ASSY IAW AMM TASK 25-62-44-400-00
- [SDR CALA2025110911021](https://openairdocs.org/sdr/CALA2025110911021.md): Elec Connector · damaged · Nov 7, 2025 · N899UA · Airbus A319132 · Light System Wiring
  > EPSU INT LOAD FWD L MSG DURING CABIN EMERGENCY LIGHT TEST PERFORMED WIRE CHECKS PER ASM 33-51-01 SCH 01, PAGE 169. FOUND RESISTANCE AT PIN T OF 10WL EPSU CONNECTOR TO GROUND TO BE 27K OHMS. SUSPECT BAD LIGHT INSIDE ESCAPE SLIDE FWD DOOR LH. REMOVED ESCAPE SLI
- [SDR CALA2025092409199](https://openairdocs.org/sdr/CALA2025092409199.md): Battery Pack · no test · Sep 23, 2025 · N899UA · Airbus A319132 · Emergency Lighting
  > EPSU UNIT EMERGENCY LIGHT L AND R TEST FAILED. REMOVED AND REPLACED LEFT AND RIGHT EPSU BATTERY UNITS. REF AMM 33-51-38. EMERGENCY POWER SUPPLY UNIT BITE CHECK NORMAL. REF AMM 33-51-00-710-001-A; CIDS BITE TEST NORMAL. REF AMM 23-73-00-740-005-A.
- [SDR CALA2025031402813](https://openairdocs.org/sdr/CALA2025031402813.md): Switch · malfunctioned · Mar 14, 2025 · N899UA · Airbus A319132 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS ON WITH SWITCH OFF ON ARMED CYCLED SWITCH.
- [SDR CALA2024120201367](https://openairdocs.org/sdr/CALA2024120201367.md): Unknown · odor · Nov 29, 2024 · N899UA · Airbus A319132 · Air Distribution System
  > FUMES IN THE COCKPIT ON DESCENT. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN. CREW REPORTED ODOR IN THE FLIGHT DECK THA T SMELLED LIKE PAINT OR LACQUER ON DESCENT INTO CHS. NO ODOR PRE SENT ON ARRIVAL TO ACFT. SUSPECT ODOR WAS FROM AN EXTERNAL SOURC E. COMP
- [SDR CALA2024042301205](https://openairdocs.org/sdr/CALA2024042301205.md): Bypass Valve · failed · Apr 20, 2024 · N899UA · Airbus A319132 · Cabin Cooling System
  > RAPID DEPRESSURIZATION OR EMERGENCY DESCENT. SLOW DEPRESSURIZATION AT FL360 EMERGENCY DESCENT. SCREEN FOUND DUCT BLOWN OFF OF VALVE BYPASS ON NR 2 PACK. AND THE SEAL THAT GOES ALONG WITH IT, THE BYPASS VALVE WAS R & R IAW AMM 21-61-53/401 CONFIG 00. PERFO
- [SDR CALA2024012900235](https://openairdocs.org/sdr/CALA2024012900235.md): Fitting · cracked · Jan 25, 2024 · N899UA · Airbus A319132 · Fuselage Main, Attach Fittings
  > FLIGHT DECK FR4 WINDSHIELD CENTER POST LOWER STRUCTURE L/H CONTI NUITY FITTING PRODUCED CRACK INDICATIONS DURING HFEC INSPECTION PER HAECO LCQ N/R 9290288/42288 GEN BY V061690 LH & RH CONTINUITY FITTING HAS BEEN REPLACED IAW ECRA V914231 INSPECTED BY LC 04 AND
- [SDR CALA2024012900236](https://openairdocs.org/sdr/CALA2024012900236.md): Window Frame · cracked · Jan 24, 2024 · N899UA · Airbus A319132 · Fuselage Main, Structure
  > FR4 WINDSHIELD CTR POST LOWER NODE LH IB HOLE HAS CRACK INDICA TION AT LOWER FACE EXTENDING FWD.020 PER HAECO LCQ N/R 9290577/ 42577 GEN BY V892444 SH INITIAL INSPECTION PER PART 2 OF THE LATEST REVISION OF ECRA REPEAT INSPECTION AT INTERVALS NOT TO EXCEED 61
- [SDR CALA2024012400208](https://openairdocs.org/sdr/CALA2024012400208.md): Intercostal · cracked · Jan 19, 2024 · N899UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > L1 DOOR STOP #7 UPPER INBD BOLT HOLE PRODUCED CRACK INDICATIONS IN THE INTERCOSTAL AT THE 3,4 AND 5:00 POSITIONS AND THE LOWER INBD BOLT HOLE PRODUCED CRACK INDICATIONS IN THE INTERCOSTAL AT THE 2:00 POSITION FR16 PER NR9290266/42266. PERFORMED REPAIR IAW R-D
- [SDR CALA2024012400207](https://openairdocs.org/sdr/CALA2024012400207.md): Door Frame · cracked · Jan 19, 2024 · N899UA · Airbus A319132 · Fuselage Main, Structure
  > L1 DOOR STOP #1 AT FR16 LOWER INBD BOLT HOLE PRODUCED CRACK INDICATIONS AT THE 3:00 AND 8:00 POSITION PER NR9290267/42267 GEN BY V061690 NITIAL INSP ON THE LH FR16 DOORSTOP FITTING #1 HOLES 3 AND 4 PER FT REACHES 37,546 TOTAL ACFT FC. PERFORM REPEAT INSP AT IN
- [SDR CALA2024012200174](https://openairdocs.org/sdr/CALA2024012200174.md): Intercostal · cracked · Jan 19, 2024 · N899UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > R1 FR16 DOOR STOP #7 UPPER INBD BOLT PRODUCED CRACK INDICATIONS IN THE INTERCOSTAL AT THE 6:00 POSITION AND IN THE FRAME AT 11:0 0 POSITION LOWER INBD HOLE PRODUCED CRACK INDICATIONS IN THE INT ERCOSTAL AT 6:00 POSITION IN THE FRAME PER NR9290268/42268.
- [SDR CALA2024012200173](https://openairdocs.org/sdr/CALA2024012200173.md): Door Frame · cracked · Jan 19, 2024 · N899UA · Airbus A319132 · Fuselage Main, Structure
  > R1 FR16 DOOR STOP #1 LOWER INBD BOLT PRODUCED CRACK INDICATIONS IN THE FRAME AT THE 12:00 POSITION AND AT 6:00 POSITION, PER NR9 290271/42271 PERFORMED REPAIR IAW A319 R-DWG R53113118 REV F CAT A REPAIR NO FURTHER RE-INSPECT REQUIRED.
- [SDR CALA2024012200169](https://openairdocs.org/sdr/CALA2024012200169.md): Stop Fitting · cracked · Jan 19, 2024 · N899UA · Airbus A319132 · Fuselage Main, Structure
  > R1 FR20 DOOR STOP #1 UPPER INBD BOLT PRODUCED CRACK INDICATIONS IN THE FRAME AT THE 6:00 POSITION LOWER INBD HOLE PRODUCED CRACK INDICATIONS IN THE FRAME AT 9:00 POSITION PER NR9290270/42270 PERFORMED REPAIR IAW A319 R-DWG R53113118 REV F CAT A REPAIR NO FURTH
- [SDR CALA2024011200084](https://openairdocs.org/sdr/CALA2024011200084.md): Stringer · corroded · Jan 11, 2024 · N899UA · Airbus A319132 · Fuselage Main, Longeron/Stringer
  > AFT CARGO DOOR FLOOR STRUCTURE, FR52 THROUGH FR54 LH STR.42 CORROSION PER NR9290527/42527. PERFORMED STRINGER SPLICE REPAIR IAW A319 R1-R534-70620_F CAT A REPAIR. NO REINSPECT REQUIRED.
- [SDR CALA2024010800051](https://openairdocs.org/sdr/CALA2024010800051.md): Threshold · corroded · Jan 3, 2024 · N899UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > AFT CARGO FLOOR STRUCTURE FR56 THROUGH FR58 DOOR SEAL SUPPORT STRUCTURE MULTIPLE FLAGGED SPOTS OF CORROSION PER NR9290533/42533 GEN BY V920443 RMVD AND RPLD AFT CARGO THRESHOLD AT FR56-58 AND REAPPLIED PROTE CTIVE COATINGS IAW SRM 51-72-11-911/001, 51-42-11/00
- [SDR CALA2024010200008](https://openairdocs.org/sdr/CALA2024010200008.md): Stringer · corroded · Dec 29, 2023 · N899UA · Airbus A319132 · Fuselage Main, Longeron/Stringer
  > AFT CARGO FLOOR STRUCTURE FR64 THROUGH FR 65 RH STR 31 EXFOLIATION/CORROSION.. REMOVED AND REPLACED STR 31RH FR 64 TO 66.9" AFT CARGO FLOOR STR PERFORMED BY V932428 AND INSP BY V892285. UCTURE IAW A319 SRM 51-42-11/001. FOUND STR 31RH FR 64 THROUGHT FR65 OUT
- [SDR CALA2023122903755](https://openairdocs.org/sdr/CALA2023122903755.md): Fitting · corroded · Dec 27, 2023 · N899UA · Airbus A319132 · Cargo/Baggage Doors
  > FWD CARGO DOOR AFT ECCENTRIC BOLT FITTING FWD LUG FWD FACE HAS CORROSION AT BUSHING BORE PER HAECO LCQ NON ROUTINE 9290415/42415 GENERATED BY N078625
- [SDR CALA2023122903753](https://openairdocs.org/sdr/CALA2023122903753.md): Floor Support · corroded · Dec 27, 2023 · N899UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > FWD CARGO THRESHOLD STILL PLATE FR24.5-28 HAS CORROSION THROUGHO UT (A3NB-53-3-6105) PER HAECO LCQ NON ROUTINE 9290462/42462 GENE RATED BY N078625
- [SDR CALA2023122203716](https://openairdocs.org/sdr/CALA2023122203716.md): Door Sill · corroded · Dec 21, 2023 · N899UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > R2 DOOR CUTOUT SILL CENTER SHAPE HAS MULTI AREAS OF CORROSION. REMOVED AND REPLACED R2 DOOR CUTOUT SILL CENTER SHAPE IAW A319 S RM 51-72-11.
- [SDR CALA2023122203715](https://openairdocs.org/sdr/CALA2023122203715.md): Door Sill · damaged · Dec 21, 2023 · N899UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > L2 DOOR CUTOUT SILL, IB OF AFT GRIT BAR FITTING IB AFT HOLE SILL BENT PER NR9290445/42445. REPAIRED L2 DOOR CUTOUT SILL IB OF AFT GRIT BAR FITTING IB AFT H OLE SILL IAW SRM 53-41-14-300-001 FIG 1.
- [SDR CALA2023121503649](https://openairdocs.org/sdr/CALA2023121503649.md): Intercostal · cracked · Dec 8, 2023 · N899UA · Airbus A319132 · Emergency Exits
  > LH OW EMERG HATCH LOAD TRANSMITTING PROFILE IS CRACKED PER 92901 85/42185. RMVD AND RPLD LOAD TRANSMITTING PROFILE ON LH WING EMERGENCY EXIT HATCH RE-APPLIED SURFACE PROTECTION IAW SRM 51-72-11-911-001, 51-42-11 & 51-75-12/001
- [SDR CALA2023012700230](https://openairdocs.org/sdr/CALA2023012700230.md): Power Supply · inoperative · Jan 27, 2023 · N899UA · Airbus A319132 · Emergency Lighting
  > EMER EXIT LIGHTS ON INAFT GALLEY OVER BOTHDOORS AND LAV. REPLACED 13WL EPSU AND BATTERY PER AMM 31-51-38-000-001-A. PARTS USED: 31-3350-9-9001, ACP VERIFICATION EMER LIGHTS NOW WORK AND NEW BOX SYS TEST OK. IDT INSPECTED PER GMM 09-10-05.
- [SDR CALA2022071101710](https://openairdocs.org/sdr/CALA2022071101710.md): None · odor · Jul 11, 2022 · N899UA · Airbus A319132 · Airborne Auxiliary Power Unit (APU) System
  > AIRCRAFT FLIGHT DECK ANDCABIN AIR STRONG ODOR LOOKING INTO TSM 05-50-00-810-831-A AND AMM 36-10-00-615-801-A. ALSO COULD CHANGE CABIN CARTARAGE RETURN FILTERS, M&E 31-2121-3-0008. SMELL VARIES IN CABIN WITH APU/PACKS RUNNING AND/OR PCAIR OIL LEAK APPEARS TO BE
- [SDR CALA2021053100767](https://openairdocs.org/sdr/CALA2021053100767.md): Clamp · missing · May 31, 2021 · N899UA · Airbus A319132 · Exterior Lighting
  > PDA 3 REF LOGPAGE #6349863 RH LANDING LIGHT CLAMP MISSING. THIS ITEM IS CONSIDERED A CLASS 3 PDA. RPREPLACED RING AND SCREW INSTALLED PER AMM 33 -42-11-01A ALSO NOTIFED AIRPORT OPS AND PREFORMED RAMP INSPECTION.
- [SDR CALA2019031100398](https://openairdocs.org/sdr/CALA2019031100398.md): Fastener · missing · Mar 11, 2019 · N899UA · Airbus A319132 · Fuselage Main, Plate/Skin
  > FASTENER MISSING ON LEADING EDGE CORNER OF PNL 196BB UPDATED MAA CODE FIX USING VENDOR MAA SCREEN CALL TOMC 847-700-9980 MM 53-35-00-200-002A. CANNOT BE MISSING FROM CORNER FOR CARRY. V ACCESS DOOR 196BB IS ATTACHED TO BELLY FAIRING PANEL 196AB REF A ARGAS TOM
- [SDR CALA2019020800231](https://openairdocs.org/sdr/CALA2019020800231.md): Limit Switch · stuck · Feb 8, 2019 · N899UA · Airbus A319132 · Potable Water System
  > FA REPORT WATER LEAKINGFROM BOTH FWD/AFT GALLEYWATER QNTY 100 AT T/OLEAK TO 0 CHECKED POTABLE WATER SYSTEM PER TSM 38-12-00-810-815A. DRAINED AND FILLED TANK AND VERIFIED QUANTITY INDICATION CORRECT. PRESSURIZED TANK AND LEAK CHECKED ALL GALLEY AND LAV WATER
- [SDR CALA2018021600628](https://openairdocs.org/sdr/CALA2018021600628.md): Frame · corroded · Feb 14, 2018 · N899UA · Airbus A319132 · Fuselage Main, Frame
  > AFT CARGO DOOR LOWER CUT OUT FRAME SUPPORT AT FRAME 59, STRINGERS 37 - 38R HAS CORROSION. REPAIRED IAW ECRA 5341-011161.
- [SDR CALA2018020900516](https://openairdocs.org/sdr/CALA2018020900516.md): Threshold · corroded · Feb 8, 2018 · N899UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY, FRAMES 55 - 59, RT DOOR THRESHOLD HAS SURFACE CORROSION. REMOVED AND REPLACED THE THRESHOLD IAW SRM 5 1-42-11.
- [SDR CALA2018012600308](https://openairdocs.org/sdr/CALA2018012600308.md): Hinge Fitting · corroded · Jan 25, 2018 · N899UA · Airbus A319132 · Landing Gear Doors
  > LEFT MLG DOOR FWD FITTING ON KEEL BEAM FWD LUG, FWD FACE HAS CORROSION. CORROSION EXCEEDS MANUFACTURE DRAWING TOLERANCES IAW IAW SRM 53 -36-11 DRAWING, 4-3 SHEET. INSTALLED A NEW HINGE FITTING IAW SRM 51-72-11, PG 2, PARA D-1.
- [SDR CALA2018011900213](https://openairdocs.org/sdr/CALA2018011900213.md): Web · corroded · Jan 16, 2018 · N899UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > FORWARD CARGO BAY, BETWEEN FRAMES 25 - 27 DOOR SILL WEB HAS THREE SPOTS OF CORROSION ON UPPER SURFACE, BELOW TIE DOWN FITTINGS. REMOVED AND REPLACED THE WEB IAW SRM 51-42-11, PARA 2.E, PARA 2.F.
- [SDR CALA2018011400191](https://openairdocs.org/sdr/CALA2018011400191.md): Stringer Splice · corroded · Jan 14, 2018 · N899UA · Airbus A319132 · Fuselage Main, Longeron/Stringer
  > AFT CARGO BAY, FRAMES 63 - 64 STRINGER SPLICE 42L HAS SURFACE CORROSION. REMOVED AND REPLACED THE STRINGER SPLICE IAW SRM 51- 42-11, PARA F.
- [SDR CALA2018011300181](https://openairdocs.org/sdr/CALA2018011300181.md): Longeron Splice · corroded · Jan 11, 2018 · N899UA · Airbus A319132 · Fuselage Main, Longeron/Stringer
  > AFT CARGO BAY STRINGER SPLICE 40L, FRAMES 63 - 64 HAS SURFACE CORROSION. REMOVED AND REPLACED THE STRINGER SPLICE IAW SRM 51-42-11, PARA F.
- [SDR CALA2018011300180](https://openairdocs.org/sdr/CALA2018011300180.md): Longeron Splice · corroded · Jan 11, 2018 · N899UA · Airbus A319132 · Fuselage Main, Longeron/Stringer
  > AFT CARGO BAY STRINGER SPLICE 43L, FRAMES 63 - 64 HAS SURFACE CORROSION. REMOVED AND REPLACED THE STRINGER SPLICE IAW SRM 51-42-11, PARA F.
- [SDR CALA2018011300179](https://openairdocs.org/sdr/CALA2018011300179.md): Stringer Splice · corroded · Jan 11, 2018 · N899UA · Airbus A319132 · Fuselage Main, Longeron/Stringer
  > AFT CARGO BAY FRAMES 63 - 64 STRINGER SPLICE 41L HAS SURFACE CORROSION. REMOVED AND REPLACED THE STRINGER SPLICE IAW SRM 51-42-11, PARA F.
- [SDR CALA2018011200137](https://openairdocs.org/sdr/CALA2018011200137.md): Shear Web · corroded · Jan 11, 2018 · N899UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > RIGHT SIDE SHEAR WEB BETWEEN FRAMES 69 & 70, HAD SEVERAL AREAS OF CORROSION ON TOP & BOTTOM SIDES. REMOVED AND REPLACED THE SHEAR WEB AND FRAME SUPPORT IAW SRM 51 -42-11, PG 2, STEP 2 A-H.
- [SDR CALA2018011200136](https://openairdocs.org/sdr/CALA2018011200136.md): Fitting · corroded · Jan 11, 2018 · N899UA · Airbus A319132 · Fuselage Main, Attach Fittings
  > R2 DOOR SILL HAS CORROSION AT FRAME 68 INBD & OTBD. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS, INSTALLED A NEW FITTING IAW SRM 51-72-11-911-001, & 51-42-11-001.
- [SDR CALA2018011200135](https://openairdocs.org/sdr/CALA2018011200135.md): Fitting · corroded · Jan 11, 2018 · N899UA · Airbus A319132 · Fuselage Main, Attach Fittings
  > R2 DOOR SILL AFT CORNER FITTING AT FRAME 68 HAS CORROSION. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. REPLACED THE CORNER FITTING IAW SRM 51-72-11-911-001 & 51-42-11-001.
- [SDR CALA2018011200133](https://openairdocs.org/sdr/CALA2018011200133.md): Fitting · corroded · Jan 11, 2018 · N899UA · Airbus A319132 · Fuselage Main, Attach Fittings
  > R2 DOOR SILL HAS CORROSION ON FWD CORNER FITTING AT FRAME 66. REMOVED CORROSION, AND FOUND TO BE OUT OF LIMITS. INSTALLED A NEW CORNER FITTING IAW SRM 51-72-11-911-001, & 51-4 2-11-001.
- [SDR CALA2018011200124](https://openairdocs.org/sdr/CALA2018011200124.md): Door Sill · corroded · Jan 8, 2018 · N899UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > L2 DOOR SILL HAS CORROSION INBD SIDE OF FRAME 66. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-72-11, PARA 2.
- [SDR CALA2018011200123](https://openairdocs.org/sdr/CALA2018011200123.md): Fitting · corroded · Jan 8, 2018 · N899UA · Airbus A319132 · Fuselage Main, Attach Fittings
  > L2 DOOR SILL HAS CORROSION ON FWD CORNER FITTING AT FRAME 66. REMOVED AND REPLACED THE FITTING IAW SRM 51-72-11, PARA 2.
- [SDR CALA2018011200122](https://openairdocs.org/sdr/CALA2018011200122.md): Fitting · corroded · Jan 8, 2018 · N899UA · Airbus A319132 · Fuselage Main, Attach Fittings
  > L2 DOOR SILL AFT CORNER FITTING HAS CORROSION AT FRAME 68. REMOVED AND REPLACED THE DOOR SILL AFT FITTING IAW SRM 51-72-11.
- [SDR CALA2018010500032](https://openairdocs.org/sdr/CALA2018010500032.md): Shear Web · corroded · Jan 4, 2018 · N899UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > LEFT SIDE SHEAR WEB 3 INCHES AND 7 INCHES FORWARD OF FRAME 70 SEVERAL AREAS OF CORROSION ON TOP AND BOTTOM SIDES OF SHEAR WEB. REMOVED AND REPLACEDTHE SHEAR WEB AND SUPPORT IAW SRM 51-42-11 REV.

## 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 = 'N899UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N899UA/reports

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