# Service difficulty reports: JASC 5343

A list on [JASC 5343](https://openairdocs.org/jasc/5343.md).

Reports filed under 5343 · Fuselage, Landing Gear Attach Fittings, newest first.

Page 1 of 39 · 1,946 reports

- [SDR JGVR20261021001](https://openairdocs.org/sdr/JGVR20261021001.md): Fitting · corroded · Oct 21, 2026 · N676QS · Cessna 680A
  > REMOVED THE CORRODED NOSE LANDING GEAR ACTUATOR FITTING ASSEMBLY AND INSTALLED NEW FITTING IAW STANDARD REPAIR.
- [SDR DALA2026102105778](https://openairdocs.org/sdr/DALA2026102105778.md): Anchor Fitting · corroded · Oct 20, 2026 · N362NW · Airbus A320212
  > LOWER FUSELAGE, LT MLG ANCHORAGE FITTING WITH CORROSION. REPAIRED LT MLG ANCHORAGE FITTING UPPER AND LOWER BEARING FACES, LUG BORE AND EDGE CHAMFERS I.A.W. SRM 57-26-13-300-008 REV.159 DATED 15 SEP, 26. THIS IS A REPAIR CATEGORY C. REPAIR LIFE LIMIT AT 48000
- [SDR UIEA2026092300914](https://openairdocs.org/sdr/UIEA2026092300914.md): Fitting · corroded · Sep 25, 2026 · N404KZ · Boeing 747481F
  > DURING THE REMOVAL OF THE RH BODY GEAR AND THE 4 BOLTS THAT HOLD THE INBOARD TRUNNION BEARING, FOUND THE LOWER BEARING CAP WITH FRETTING CORROSION IN THE INBOARD SIDE.(<P>ACCOMPLISHED MAJOR REPAIR/REPLACEMENT OF RH BODY LANDING GEAR LOWER BEARING CAP DUE TO TH
- [SDR AALA202609153681](https://openairdocs.org/sdr/AALA202609153681.md): Trunnion · corroded · Sep 12, 2026 · N937NN · Boeing 737823
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON NLG LT INBOARD TRUNNION FITTINGS. MAINTENANCE REPLACED NLG LT INBOARD TRUNION FITTINGS IAW EA 378675.
- [SDR DALA2026091305107](https://openairdocs.org/sdr/DALA2026091305107.md): Anchor Fitting · corroded · Sep 9, 2026 · N353NW · Airbus A320212
  > LEVEL 2 CORROSION, LOWER FUSELAGE, RT MLG ANCHORAGE FITTING WITH CORROSION. REPAIRED RH MLG RETRACTION JACK ANCHORAGE FITTING LUG BARE, UPPER AND LOWER BEARING FACES AND EDGE CHAMFER I.A.W. A320 SRM TASK 57-26-13-300-008 REV. 158 DATED 01 JUN, 26. THIS IS REP
- [SDR DALA2026091305106](https://openairdocs.org/sdr/DALA2026091305106.md): Anchor Fitting · corroded · Sep 9, 2026 · N353NW · Airbus A320212
  > LEVEL 2 CORROSION, LOWER FUSELAGE, LH MLG ANCHORAGE FITTING WITH CORROSION. C/A: REPAIRED LH MLG RETRACTIION JACK ANCHORAGE FITTING LUG BARE UPPER AND LOWER BEARING FACES AND EDGE CHAMFER I.A.W. A320 SRM TASK 57-26-13-300-008 REV. 158 DATED 01 JUN, 26. THIS IS
- [SDR CALA2026091419399](https://openairdocs.org/sdr/CALA2026091419399.md): Fitting · damaged · Sep 4, 2026 · N14704 · Boeing 737724
  > REMOVED AND REPLACE NLG RETRACT ACTUATOR FITTING DAMAGED, P/N: 141A7650-2. REMOVED AND REPLACED NLG RETRACT ACTUATOR FITTING ALL WORK DONE IAW SRM 51-40-02-0G-0, SRM 51-40-05-0G-0, DWG 141A7001 REV A. REMOVED AND REPLACED NLG RETREACT ACTUATOR FITTING ALL WO
- [SDR 2026F00184](https://openairdocs.org/sdr/2026F00184.md): Fitting · corroded · Aug 25, 2026 · N622QS · Cessna 680A
  > REMOVED NOSE LANDING GEAR ACTUATOR FITTING ASSEMBLY DUE TO LEVEL 2 CORROSION. INSTALLED NEW FITTING PER SR-680A-ATA53-33739 REV. A, STANDARD REPAIR - NLG ACTUATOR FITTING REPLACEMENT, DATED 28 NOV 2023. SUPPORTED BY 8100-9 FORM DATED 29 NOV 2023.
- [SDR DALA2026073004396](https://openairdocs.org/sdr/DALA2026073004396.md): Bushing · migrated · Jul 29, 2026 · N106DN · Airbus A321211
  > MIGRATED BUSHING AFT LUG RH MLG ACTUATOR FITTING. CORRECTIVE ACTION: REPAIRED PER ERA 635754-14AD REV ORIGINAL. (1727287) AIRCRAFT WAS GROUNDED.
- [SDR UIEA2026071200589](https://openairdocs.org/sdr/UIEA2026071200589.md): Bushing · damaged · Jul 29, 2026 · N485MC · Boeing 74745EF
  > REWORK RH BLG I/B TRUNNION BUSHINGS(<P>PERMANENT REPAIR TO USE BAC5701 TYP 11 CL2 IN LIEU OF SOPM 20-42-05 TYP 11 CL2 AS PER RI-32-13-18363 REV B. NO FURTHER DEFECTS NOTED </P>)
- [SDR UIEA2026071200591](https://openairdocs.org/sdr/UIEA2026071200591.md): Bushing · damaged · Jul 29, 2026 · N485MC · Boeing 74745EF
  > REWORK LH BLG I/B TRUNNION BUSHING(<P>PERMANENT REPAIR TO USE BAC5701 TYP 11 CL2 IN LIEU OF SOPM 20-42-05 TYP 11 CL2 AS PER RI-32-18362 REV B. NO FURTHER DEFECTS NOTED</P>)
- [SDR UIEA2026071200592](https://openairdocs.org/sdr/UIEA2026071200592.md): Bearing Race · damaged · Jul 29, 2026 · N485MC · Boeing 74745EF
  > REWORK LH BLG O/B TRUNNION BEARING RACE(<P>PERMANENT REPAIR TO USE BAC5701 TYP 11 CL2 IN LIEU OF SOPM 20-42-05 TYP 11 CL2 AS PER RI-32-13-18385 REV B. NO FURTHER DEFECTS NOTED </P>)
- [SDR 2026FA0000610](https://openairdocs.org/sdr/2026FA0000610.md): Fork · cracked · Jul 29, 2026 · N88765 · Dhav DHC3
  > CRACKED TAIL LANDING GEAR FORK PART NUMBER C3UT85-3. CRACK IN CRITICAL AREA OF FORK WHERE FAILURE COULD CAUSE MAJOR DAMAGE TO AIRCRAFT DURING TAKE OFF OR LANDING. ORIGINAL OEM CAST TAIL FORK FAILS AND BREAKS WHICH FORCES TAIL LANDING GEAR WITH TAIL SKI TO CO
- [SDR FDEA202607291054](https://openairdocs.org/sdr/FDEA202607291054.md): Trunnion · cracked · Jul 29, 2026 · N605FE · Doug MD11F
  > DURING HIGH FREQUENCY EDDY CURRENT INSPECTION ON NOSE LANDING GEAR RIGHT TRUNNION FITTING AT STATION 595 EXISTING REPAIR SLOT OUT AREA FOUND 01EA CRACK WITH LENGTH APPROX. 1/4". CRACK AREA AT NOSE LANDING GEAR RIGHT HAND TRUNNION FITTING STATION 595 EXIST
- [SDR 2026FA0000606](https://openairdocs.org/sdr/2026FA0000606.md): Rib · cracked · Jul 28, 2026 · N1342G · Cessna 310R
  > LEFT AND RIGHT MAIN LANDING GEAR SIDE BRACE RIBS CRACKED PER CESSNA ME76-2
- [SDR 2026FA0000592](https://openairdocs.org/sdr/2026FA0000592.md): Bushing · delaminated · Jul 12, 2026 · N636EM · Cessna 172S
  > BOTH LANDING GEAR BUSHING FOUND DELAMINATED DURING 100HR INSPECTION.
- [SDR IPXA2026062629173](https://openairdocs.org/sdr/IPXA2026062629173.md): Support Fitting · corroded · Jun 24, 2026 · N429UP · Boeing 75724APF
  > (APG) RT AFT TRUNNION SUPPORT FITTING BEARING ASSY INSIDE HOUSING HAS CORROSION. INSTALLED SERVICEABLE BEARING ASSY R/H AFT TRUNNION SUPPORT FITTING IAW AMM 57-54-07-404-036
- [SDR IPXA2026062629263](https://openairdocs.org/sdr/IPXA2026062629263.md): Bearing · corroded · Jun 24, 2026 · N429UP · Boeing 75724APF
  > LEFT AFT TRUNNION SUPPORT FITTING BEARING ASSY INSIDE HOUSING HAS CORROSION INSTALLED SERVICIABLE BEARING ASSY AT LT AFT TRUNNION SUPPORT FITTING IAW AMM 57-54-07-404-036.
- [SDR DXTA2026061908479](https://openairdocs.org/sdr/DXTA2026061908479.md): Link Pin · corroded · Jun 16, 2026 · N601QS · Cessna 680A
  > WEAR AND CORROSION ON LT MLG TRAILING LINK PIN FOUND DURING MAIN LANDING GEAR TRUNNION, TRAILING LINK, AND LINK PIN DETAIL INSPECTION
- [SDR IPXA2026052660648](https://openairdocs.org/sdr/IPXA2026052660648.md): Trunnion · damaged · May 26, 2026 · N632UP · Boeing 7478F
  > RIGHT BODY GEAR TRUNION OUTBOARD BUSHING MIGRATING OUT AND APPEARS TO HAVE AXIAL SPLIT AT FORWARD 90 DEGREE POSITION. GA TELESIS REPAIRED MIGRATING BUSHING ON 8130 FORM TRACKING NUMBER WO450757 DOCUMENT ATTACHED. GEAR R & R ON MXP-32-410-90-02-JIC ((RII) RST -
- [SDR SWIA2026051777306](https://openairdocs.org/sdr/SWIA2026051777306.md): Trunnion · gouged · May 17, 2026 · N936SW · Cndair CL6002B19
  > RH SIDE AFT TRUNNION HAS GOUGE MARKS ON FWD FACE. REPAIRED GOUGE DAMAGE TO THE MLG TRUNNION FITTING NEAR AFT LUG BORE, RT IAW REO 601R-57-21-4093, REV -.
- [SDR SWIA2026050977288](https://openairdocs.org/sdr/SWIA2026050977288.md): Skin · damaged · May 9, 2026 · N936SW · Cndair CL6002B19
  > LEFT APRON SKIN PANEL ASSY HAD CHAFE AND GOUGE DAMAGE. REPAIRED THE APRON ASSY SKIN PANEL, IAW REO 601R-53-41-3446, REV-.
- [SDR DALA2026042102517](https://openairdocs.org/sdr/DALA2026042102517.md): Block · corroded · Apr 18, 2026 · N866DN · Boeing 737932ER
  > LEFT MLG H-BLOCK HAVE PITTING ON UPPER I/B AND O/B AND LOWER I/B AND O/B ON BUSING FACE. REPLACED LMLG FWD TRUNNION HOUSING ASSEMBLY PER B737 AMM 57-16-01. (LOG 1551203 - AIRCRAFT WAS GROUNDED).
- [SDR SWIA2026041677291](https://openairdocs.org/sdr/SWIA2026041677291.md): Trunnion · cracked · Apr 16, 2026 · N936SW · Cndair CL6002B19
  > COMPLY WITH SCHEDULED MAINTENANCE CODE RA18382-601R-57-21-1703-PR. COMPLY WITH PERMANENT REPAIR ON RA ID 183824. FASTNER HOLES IN LT MLG TRUNNION ARE CRACKED. REPAIRED IAW REO 601R-57-21-1703, REV -. REPLACED THE LT TRUNNION MLG AND STEEL STRAP POST SB 60
- [SDR 2026FA0000266](https://openairdocs.org/sdr/2026FA0000266.md): Bearing · broken · Apr 13, 2026 · N445BG · Piper PA44180
  > FOUND THE LEFT AND RIGHT HAND OUTBOARD NOSE GEAR TRUNNION ASSY BEARINGS BROKEN AT THEIR FLANGES RESULTING IN MUCH SIDE-TO-SIDE PLAY IN THE NOSE LANDING GEAR. INSPECTION OF THE O.D. OF THE TRUNNION ASSY IN WHICH THE BEARINGS ARE INSTALLED WAS IN TOLERANCE. NO O
- [SDR REXA2026050700499](https://openairdocs.org/sdr/REXA2026050700499.md): Fitting · corroded · Mar 15, 2026 · N138EV · Cndair CL6002D24
  > CORROSION WAS FOUND ON FITTINGS LH/RH SIDE AT AFT NOSE LANDING GEAR DOOR AND ALSO ON FUSELAGE STRUCTURE (4EAS). FITTINGS LH/RH SIDE AT AFT NOSE LANDING GEAR DOOR AND ALSO ON FUSELAGE STRUCTURE (4EAS) WERE REPLACED PER CRJ900 SRM 51-42-
- [SDR U5OA2026031200179](https://openairdocs.org/sdr/U5OA2026031200179.md): Mount · cracked · Mar 12, 2026 · N999AA · Gulstm GIV
  > PILOTS NEEDED TO BLOW DOWN THE LANDING GEAR BECAUSE THE NOSE GEAR WOULD NOT COME DOWN AND LOCK (UNDER NORMAL OPERATION). MAINTENANCE INITIAL EVALUATION FOUND THAT THE NOSE GEAR UPLOCK ROLLER WAS NOT ENGAGING WITH THE UPLOCK. FURTHER INVESTIGATION FOUND MOVEMEN
- [SDR HNAA2026032600241](https://openairdocs.org/sdr/HNAA2026032600241.md): Bearing · corroded · Mar 1, 2026 · N699AE · Emb EMB145LR
  > RE-EVALUATE PREVIOUSLY BLENDED AREAS ON LT NLG LEG TRUNNION BEARING RACE. R & R THE LT NLG TRUNNION IAW ETD2026-145-004079 AND EO #EO1-53-26-0126
- [SDR HNAA2026032600245](https://openairdocs.org/sdr/HNAA2026032600245.md): Trunnion · damaged · Feb 12, 2026 · N644AE · Emb EMB145LR
  > RIGHT NLG BEARING HOUSING HAS TEMPORARY REPAIR IAW ETD2023-145-026080A REQUIRES REPLACEMENT. R & R THE RT NLG TRUNNION IAW ETD2023-145-026080 REV. A AND PIEDMONT EO1-53-26-0127 DMT 10.
- [SDR UIEA2026013000021](https://openairdocs.org/sdr/UIEA2026013000021.md): Trunnion · corroded · Feb 5, 2026 · N439GT · Boeing 747409F
  > LEFT BODY GEAR INBOARD TRUNNION, AIRCRAFT SIDE HAS CORROSION. BLENDED AREA ON LT BODY GEAR INBD TRUNNION. PERFORMED NDT AND DVI INSP. NO DEFECTS NOTED. ACCOMPLISHED FLAP PEEN, APPLIED TREATMENT, PRIMER & TOPCOAT IAW SRM 53-40-90-2R-1, REP 1, PAGE 7. COMPLYE
- [SDR UIEA2026013000022](https://openairdocs.org/sdr/UIEA2026013000022.md): Trunnion · gouged · Feb 5, 2026 · N439GT · Boeing 747409F
  > GOUGE ON LT NLG TRUNNION BEARING CAP FWD AND AFT I/B CORNER. REPAIRED DAMAGE ON LT NLG TRUNNION BEARING CAP FWD AND AFT INBD CORNERS. IAW BOEING MESSAGE EA C-TLS-26-0002-10B. PERMANENT REPAIR WITH NO ADDITIONAL SUPPLEMENTAL INSPECTIONS. NO FURTHER DEFECTS NOT
- [SDR UIEA2026013000023](https://openairdocs.org/sdr/UIEA2026013000023.md): Trunnion · corroded · Feb 5, 2026 · N439GT · Boeing 747409F
  > CORROSION ON OTBD EDGE OF LT BODY GEAR TRUNNION CAP. BLENDED AREA ON OTBD EDGE OF LT BODY GEAR TRUNNION INBD CAP. PERFORMED NDT AND DVI INSP. NO DEFECTS NOTED. ACCOMPLISHED FLAP PEEN, APPLIED TREATMENT, PRIMER AND TOPCOAT PER 747 SRM 53-40-90-2R-1 REP 1 PG 7
- [SDR UIEA2026013000026](https://openairdocs.org/sdr/UIEA2026013000026.md): Trunnion · corroded · Feb 5, 2026 · N439GT · Boeing 747409F
  > CORROSION ON LT NLG TRUNNION BEARING CAP INBD SIDE. BLENDED OUT CORROSION ON THE LT NLG TRUNNION BEARING CAP INBD SIDE FACE AREA, WITHIN LIMITS. TREATED AREA PROTECTIVE FINISH ON BLENDED AREA IAW SRM 53-10-90-2R-1, REPAIR 1, FIG 201, DETAIL II. NO FURTHER DEF
- [SDR UIEA2026013000027](https://openairdocs.org/sdr/UIEA2026013000027.md): Trunnion · corroded · Feb 5, 2026 · N439GT · Boeing 747409F
  > CORROSION ON RT NLG TRUNNION BEARING CAP INBD SIDE. BLENDED OUT CORROSION ON THE RT NLG TRUNNION BEARING CAP INBD SIDE IAW SRM 51-10-90-2R-1, FIG 201. NO FURTHER DEFECTS NOTED.
- [SDR DALA2026083104896](https://openairdocs.org/sdr/DALA2026083104896.md): Bracket · corroded · Jan 18, 2026 · N654DL · Boeing 757232
  > RT MLG DOOR CENTER HINGE FWD SEAL RETAINER BRACKET CORRODED. BRACKET WIP 359055 BRACKET WAS REPLACED ON PRI 631605-14 (1408230)(AIRCRFT GROUNDED)
- [SDR FDEA202601170065](https://openairdocs.org/sdr/FDEA202601170065.md): Trunnion · fod · Jan 17, 2026 · N149FE · Boeing 7673S2F
  > AFTER LAND IN TUCSON, MAKING A HARD LEFT TURN WITH TILLER, ACFT WOULD NOT TURN. TILLER JAMMED AT 3 INDICES LT OR RT OF CENTER. AMM 32-51-00-5. COMPLIED WITH AMM 32-51-00-5, STEP 3. F. PREPARE FOR TEST OF NLG STEERING SYSTEM, G. TEST OF NLG STEERING SYS H.
- [SDR SWIA2026030975471](https://openairdocs.org/sdr/SWIA2026030975471.md): Attach Angle · corroded · Jan 9, 2026 · N779SK · Cndair CL6002C11
  > THE LH MLG WHEEL WELL FORWARD ATTACH ANGLE FOR TIRE BURST PANEL 542AZ IS CORRODED AROUND NUTPLATE HOLES. (C-CHECK RO 03/07/2026)REMOVED AND REPLACED BY NEW LH MGL WHEEL WELL FWD ANGLE COMMON TO PANEL 542AZ, REF. CRJ-550, SRM 51-42-21-001-001-A01 REV: 38 DATE
- [SDR SWIA2026030975466](https://openairdocs.org/sdr/SWIA2026030975466.md): Attach Angle · corroded · Jan 9, 2026 · N779SK · Cndair CL6002C11
  > THE RH MLG WHEEL WELL FORWARD ATTACH ANGLE FOR TIRE BURST PANEL 642AZ IS CORRODED AROUND NUTPLATE HOLES. (C-CHECK RO 03/07/2026)REMOVED AND REPLACED BY NEW RH MGL WHEEL WELL FWD ANGLE COMMON TO PANEL 642AZ, REF. CRJ-550, SRM 51-42-21-001-001-A01 REV: 38 DATE:
- [SDR IPXA2025122011655](https://openairdocs.org/sdr/IPXA2025122011655.md): Trunnion · corroded · Dec 18, 2025 · N607UP · Boeing 7478F
  > RIGHT BODY GEAR INBD TRUNNION OUTBD FACE OF UPPER TRUNNION CAP HAS CORROSION AND DAMAGE WHERE BUSHING SEATS. VERIFIED REPAIRED TO RH BODY GEAR INBD TRUNNION OUTBD FACING OF UPPER TRUNNION CAP IAW SRM 53-40-90 AND GMM 04.02.
- [SDR 2026FA0000427](https://openairdocs.org/sdr/2026FA0000427.md): Attach Fitting · debonded · Dec 12, 2025 · N408SA · Diamon DA42NG
  > ON ROLL OUT AFTER LANDING THE LH LANDING GEAR RETRACTED UNCOMMANDED CAUSING A PROPELLER STRIKE AND LH WING TIP TO TOUCH GROUND. UPON INVESTIGATION IT WAS DISCOVERED THAT THE LANDING GEAR SUPPORT BOX THAT BONDS TO THE SPAR HAD COME DETACHED FROM THE SPAR DUE TO
- [SDR JR2R20251209775](https://openairdocs.org/sdr/JR2R20251209775.md): Trunnion · chafed · Dec 9, 2025 · N89304 · Emb ERJ170200LR
  > NOSE LANDING GEAR TRUNNION BORE HAS EVIDENCE OF DAMAGE. BLEND DAMAGED AREA.
- [SDR SWIA2025120875751](https://openairdocs.org/sdr/SWIA2025120875751.md): Rib · cracked · Dec 8, 2025 · N952SW · Cndair CL6002B19
  > RIGHT MLG WHEEL WELL BATTERY RIB AT WS.48.3 HAS POSSIBLE CRACK ON FWD AND AFT END. REMOVED AND REPLACED CRACKED BATTERY RIB IN THE RT MLG WHEEL WELL IAW DWG 600-10204 REV M AND SRM 51-42-21. COMPLIED WITH 51-900-1003 SKY.
- [SDR SWIA2025120875733](https://openairdocs.org/sdr/SWIA2025120875733.md): Rib · cracked · Dec 8, 2025 · N952SW · Cndair CL6002B19
  > LEFT MLG WHEEL WELL BATTERY RIB AT WS.48.3 HAS POSSIBLE CRACK ON FWD OB END. REPAIRED THE LT BATTERY RIB WEB AT WS48.3. REO 601R-57-21-4030 REV --, COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY.
- [SDR SWIA2025112575841](https://openairdocs.org/sdr/SWIA2025112575841.md): Trunnion · cracked · Nov 25, 2025 · N959SW · Cndair CL6002B19
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA26772-601R-57-21-2287 959SW-PR - COMPLY WITH PERMANENT REPAIR ON RA ID: 267723 EA. FASTENER HOLES WERE FOUND CRACKED ON R/H MLG TRUNNION. REPAIRED REF REO 601R-57-21-2287. TRUNNION FITTING LIFE LIMIT/DISCARD TIME DUE
- [SDR 2025FA0000793](https://openairdocs.org/sdr/2025FA0000793.md): Bushing · delaminated · Nov 24, 2025 · N309TX · Cessna 172S
  > THE RIGHT LANDING GEAR LEG BUSHING WHICH SECURES THE LEG TIGHTLY TO THE AIRFRAME STRUCTURE HAD A DELAMINATED BUSHING LINER WHICH COMPLETELY WORKED ITSELF OUT OF THE BUSHING. THE LANDING GEAR LEG WAS FLOPPING AROUND INSIDE THIS BUSHING.
- [SDR SWIA2026031075487](https://openairdocs.org/sdr/SWIA2026031075487.md): Fitting · gouged · Nov 23, 2025 · N632SK · Cndair CL6002C10
  > LEFT MLG SIDE STAY FITTING GOUGED. PERFORMED BLENDED OUT AND EVALUATED AREA ON LT MLG SIDE STAY FITTING, CONDITION IS STRUCTURALLY ACCEPTABLE IAW REO 670-57-11-244, REV--, SRM 51-12-00, 51-24-11, 51-21-11, 51-25-06, 51-25-16.
- [SDR AALA202512245002](https://openairdocs.org/sdr/AALA202512245002.md): Hinge Fitting · cracked · Nov 13, 2025 · N831AW · Airbus A319132
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON MLG FWD HINGE FITTING RH SIDE, AFT LUG POSITION. CRACK LENGTH IS L= 0.180 INCH. MAINTENANCE REPLACED MLG FWD HINGE FITTING RH SIDE IAW EA 369995 AND REPAIR DWG R53370500 ISSUE F, A319 SRM 51-42-11-801 AND
- [SDR VNAA20251015091](https://openairdocs.org/sdr/VNAA20251015091.md): Fitting · damaged · Oct 17, 2025 · N501BG · Cndair CL6002C10
  > OTBD BUSHING OF THE OTBD LUG OF THE L/H FITTING FOUND TO BE DAMAGED UPON REMOVAL REPAIRED THE OUTBD LUG OF THE L/H MLG SIDE STAY FITTING IAW MHIRJ REO 670-57-11-321 REV. --, DWG CC670-10608
- [SDR VNAA20251014026](https://openairdocs.org/sdr/VNAA20251014026.md): Trunnion · elongated · Oct 14, 2025 · N501BG · Cndair CL6002C10
  > RH MLG TRUNNION HAS 5EA. ELONGATED HOLES THAT REQUIRE ENGINEERING. REPAIRED RH MLG TRUNNION REO 670-57-21-1060 REV -- DATE 2025-07-03.
- [SDR VNAA20251014025](https://openairdocs.org/sdr/VNAA20251014025.md): Trunnion · damaged · Oct 14, 2025 · N501BG · Cndair CL6002C10
  > RH MLG TRUNNION REQUIRES REPLACEMENT CORRECTIVE ACTION: INSTALLED NEW TITANIUM RH TRUNNION PN CC670-10630-4S IAW DWG KCMW670-10905

Next page: https://openairdocs.org/jasc/5343/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 jasc_code = '5343'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/jasc/5343/reports

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