# Service difficulty reports: JASC 5350

A list on [JASC 5350](https://openairdocs.org/jasc/5350.md).

Reports filed under 5350 · Aerodynamic Fairings, newest first.

Page 1 of 123 · 6,109 reports

- [SDR VNAA202610230003](https://openairdocs.org/sdr/VNAA202610230003.md): Support · corroded · Oct 23, 2026 · N546FF · Cndair CL6002C10
  > CORROSION ON FAIRING SUPPORT (FRAMES) 2 EAS STA BS 629 AND 661 AND DIAFRAGMA 1EA BTW FS 629-FS 661 (SEATLEMENT AREA, UNDER ACCESS PANELS 191 AB, 191BB AND 192BB) SUMMARY:CORROSION WAS REMOVED PER 51-42-06-001-001-A01 AREA WAS EVALUATE PER SRM 53-82-55-101-0
- [SDR AALA202610230051](https://openairdocs.org/sdr/AALA202610230051.md): Fairing · vibration · Oct 22, 2026 · N300NY · Airbus A321253NX
  > AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO ORD DUE TO THE FLIGHT ATTENDANTS REPORTING A SIGNIFICANT HUM AND VIBRATIONS FELT IN THE DECK FROM ROW 14 TO FIRST CLASS - THE AIRCRAFT LANDED SAFELY AT ORD WITHOUT FURTHER INCIDENT -
- [SDR DALA2026102105781](https://openairdocs.org/sdr/DALA2026102105781.md): Panel · missing · Oct 18, 2026 · N378NW · Airbus A320211
  > BELLY FAIRING SLIDING PANEL, LT BELLY FAIRING SLIDING PANEL MISSING. FWD TO CDL 57-00-02. "M" PROC C/W. DISPATCH APPROVED. CDL AND PLAC INSTALLED. (LP: 9191132, AIRCRAFT WAS GROUNDED)
- [SDR SWAA2026101639244](https://openairdocs.org/sdr/SWAA2026101639244.md): Radome · cracked · Oct 12, 2026 · N486WN · Boeing 7377H4
  > RADOME CRACKED AT 6 OCLOCK POSITION, R & R THE NOSE RADOME IAW AMM 53-52-00.
- [SDR DALA2026100905577](https://openairdocs.org/sdr/DALA2026100905577.md): Tail Cone · punctured · Oct 8, 2026 · N921AT · Boeing 717200
  > TAIL CONE DECAL DAMAGED & PUNCTURED, REPLACED THE DECAL IAW MM 52-20. (9388108) (AIRCRAFT GROUNDED).
- [SDR IPXA2026100957455](https://openairdocs.org/sdr/IPXA2026100957455.md): Radome · broken · Oct 2, 2026 · N364UP · Boeing 767346
  > BROKEN COMPOSITE, RADOME EXTERNAL 2 AREA. IAW EO-35385-JIC001, REV 4, INSTALL RADOME BOOT. I.A.W AMM 53-12-01-402-059 REV.149 INSTALL THE NOSE RADOME. CONDITION CHECK NORMAL.
- [SDR R61A2026092700285](https://openairdocs.org/sdr/R61A2026092700285.md): Strap · corroded · Sep 27, 2026 · N211JQ · Emb ERJ170200LR
  > WHILE AC WAS IN FOR HVY CK FOUND CORRODED FWD WTB FAIRING TO FUSELAGE STRAP FOUND ON CF1 AT FR 27-28, S28L-S24R. MX REPLACED STRAP IAW SRM 51-42-02, 51-43-04 AND 51-41-02.
- [SDR SWAA2026100529699](https://openairdocs.org/sdr/SWAA2026100529699.md): Radome · delaminated · Sep 22, 2026 · N8888M · Boeing 7378
  > NOSE RADOME HAS DELAMINATION. NOSE RADOME REPLACED ON TTG8Q01ES0U2.
- [SDR DALA2026092205299](https://openairdocs.org/sdr/DALA2026092205299.md): Radome · damaged · Sep 20, 2026 · N369NW · Airbus A320212
  > BIRD STRIKE ON RADOME ON APPROACH NO UNUSUAL INDICATION OR SMELL FOLLOWING STRIKE. C/W BIRD STRIKE INSPECTION IAW AMM 05-51-14. NO OTHER DAMAGE NOTED. STRIKE ON RADOME DEFERRED TO MON WITH COMPLETIOIN OF ERA 637070-14 REV ORIGINAL. SEC 1. PERMINENT REPAIR WIT
- [SDR CALA2026092119620](https://openairdocs.org/sdr/CALA2026092119620.md): Bracket · corroded · Sep 18, 2026 · N18112 · Boeing 757224
  > RIGHT LWR WING TO BODY FAIRING, BY THE RAM AIR INLET AT BS 880 RBL 20, ONE BRACKET CORRODED. THE BRACKET WAS REMOVED AND REPLACED AND LID WAS REMOVED AND REPLACED IAW DWG 149N7160, REV K IAW SRM 51-40-05-0G, AND SRM 51-40-05-0G.
- [SDR DALA2026092105251](https://openairdocs.org/sdr/DALA2026092105251.md): Radome · damaged · Sep 18, 2026 · N375NC · Airbus A320212
  > BIRD STRIKE ON JACCC SID NEAR L IDAS AT APPROX 6000 FT. NOSE OF A/C. CLEANED LOWER PART OF THE RADOME WHERE BIRD STRUCK. PERFORMED INSPECTION OF THE AIRCRAFT AFTER A BIRD STRIKE PER A320 AMM TASK 05-51-14-200-803-A, FOUND INTERNAL DISBONDING/DELAMINATION AND
- [SDR IPXA2026092267592](https://openairdocs.org/sdr/IPXA2026092267592.md): Fairing · debonded · Sep 16, 2026 · N355UP · Boeing 76734AF
  > DEBONDED SKIN, RT AFT WING TO BODY FAIRING LATCH PANEL 198 CR. REMOVE THE DISBOND MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH RESIN CURED AT 200°F FOR 220 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG. BOND THE FOIL WITH RESIN CURED AT 200°F FOR 220 MINUTES
- [SDR N6WA2026091803](https://openairdocs.org/sdr/N6WA2026091803.md): Support Frame · corroded · Sep 16, 2026 · N526GJ · Cndair CL6002C11
  > FRAME SUPPORT STRUCTURE RT AFT FAIRING AT FS 939 IS OUT OF LIMITS. REMOVED AND REPLACED RT FRAME SUPPORT STRUCTURE AFT FAIRING AT FS 939 IAW SRM 51-26-00.
- [SDR SWAA2026101493635](https://openairdocs.org/sdr/SWAA2026101493635.md): Access Panel · delaminated · Sep 15, 2026 · N8656B · Boeing 7378H4
  > DELAMINATED ACCESS PANEL 194CR ON BODY FAIRING. REPAIRED THE ACCESS PANEL ON THE BODY FAIRING IAW SRM 51-70-04-2R-2, REPAIR 2.
- [SDR DALA2026091805226](https://openairdocs.org/sdr/DALA2026091805226.md): Angle · cracked · Sep 15, 2026 · N595NW · Boeing 757351
  > CRACK ON ANGLES ON WING TO BODY FAIRING STRUCTURE. BS 1180+60, S26R. REPAIRED PER B757-300 SRM 51-70-11 (1813690)(AIRCRAFT GROUNDED)
- [SDR SWAA2026091677980](https://openairdocs.org/sdr/SWAA2026091677980.md): Tail Cone · delaminated · Sep 15, 2026 · N7889A · Boeing 73779L
  > DELAMINATION ON TAIL CONE AT 4 O'CLOCK. REMOVED DAMAGED SKIN IAW SRM.53-80-70-2R-1, REPAIR 1, 51-70-05-2R-11, REPAIR 11, SRM 51-70-05-2R-1, REPAIR 1. APPLIED POTTING & CURED IAW SRM.51-70-05-2R-11, REPAIR 11. APPLIED HOT BOND REPAIR TAP TEST FAILED IAW SRM.5
- [SDR DALA2026091505150](https://openairdocs.org/sdr/DALA2026091505150.md): Support · corroded · Sep 14, 2026 · N139DU · Airbus BD5001A10
  > CORROSION ON WTB FAIRING SUPPORT STRUCTURE BETWEEN FRAME 43 AND FRAME 44 AT STR 36R. C/W ER/A 636701-14 REV ORIGINAL. (LP# 1813148; AIRCRAFT WAS GROUNDED).
- [SDR DALA2026091505143](https://openairdocs.org/sdr/DALA2026091505143.md): Access Panel · corroded · Sep 14, 2026 · N345NB · Airbus A319114
  > LEVEL 2 CORROSION, APU EXHAUST TAIL CONE AT FR 86, ACCESS PANEL 317AL WERE FOUND FRAME AUXILIARY, TRANSFORMER REAR NAVIGATION LIGHT AND BONDING ANGLE WITH CORROSION AND AT FUSELAGE AREA FOUND FR 86 LOWER FRAME SECTION (CHANNEL) WITH CORROSION. (LP: 1813002, AI
- [SDR 2026FA0000692](https://openairdocs.org/sdr/2026FA0000692.md): Radome · abnormal · Sep 14, 2026 · N765JW · Cessna 525B
  > WHILE TAKING DELIVERY OF A NEW AIRCRAFT, NOTICED THE RADOME TO FUSELAGE CONTOUR HAS A MISMATCH. THE RADOME IS BIGGER THAN THE FUSELAGE. AT THE SAME TIME TEXTRON WAS DELIVERING S/N 525B-0917 AND IT HAD A LARGER MISMATCH. WAS TOLD BY TEXTRON REPRESENTATIVES TH
- [SDR DXTA2026091509690](https://openairdocs.org/sdr/DXTA2026091509690.md): Sealant · misinstalled · Sep 13, 2026 · N444QS · Emb EMB505
  > DURING DESCENT FROM AROUND FL200 A LOW LOUD HUM STARTED. WE WERE AROUND 295-300KTS VIBRATION FELT IN FEET FROM LEFT AND RIGHT PILOT. WORSE VIBRATION FELT FROM THE FLOOR INLINE WITH THE MAIN CABIN DOOR. VIBRATION AND SOUND STOPPED AT 11,000FT IN LEVEL OFF AFTER
- [SDR VNAA2026091102](https://openairdocs.org/sdr/VNAA2026091102.md): Angle · corroded · Sep 11, 2026 · N507AE · Cndair CL6002C10
  > ON AFT WING TO FUSELAGE FAIRING SUPORT STRUCTURE FOUND LT ANGLE BS 939, RT ANGLE BS 939 & ANGLE ARE CORRODED. REFERENCE SRM 53-82-55-001-002-A01 SHEET 5 OF 5 ITEMS 96, 97 AND 98). REMOVED AND REPLACED CORRODED ANGLES.
- [SDR DALA2026091605180](https://openairdocs.org/sdr/DALA2026091605180.md): Longeron · corroded · Sep 9, 2026 · N139DU · Airbus BD5001A10
  > CNTR WING TO BODY FAIRING LONGERON, BTWN FR46 AND FR48, RBL 9, BTWN FR48 AND FR52, LBL 5, CORRODED TIME LIMITED. ACCOMPLISH REPETITIVE INSPECTION PER ERA 636699-14 EVERY 1000 FH AND TERMINATING ACTION WITHIN 10,000 FH FROM 9 SEP 2026. ASSOCIATED ER/A 00-6366
- [SDR DALA2026091605178](https://openairdocs.org/sdr/DALA2026091605178.md): Longeron · corroded · Sep 9, 2026 · N139DU · Airbus BD5001A10
  > FUSELAGE, WTB FAIRING LONGERON, BETWEEN FR 48 - 52, RBL 5. CORROSION TIME LIMITED REPAIR. INSPECT THE SUBJECT AREA IAW ERA 636701-14, SEC II, EVERY 1000 FH AND TERMINATING ACTION DUE WITHIN 10,000 FH FROM REPAIR ACCOMPLISHMENT, DTE STAGE III. ASSOCIATED ER/A
- [SDR DALA2026091105090](https://openairdocs.org/sdr/DALA2026091105090.md): Support · corroded · Sep 9, 2026 · N139DU · Airbus BD5001A10
  > CORROSION ON WTB FAIRING SUPPORT STRUCTURE AT LONGERON 20" AFT OF FR48 TO FR52 LBL4. ACCOMPLISHED ER/A# 636699-14 REV-ORIGINAL. ASSOCIATED ER/A 14-636699 ADDED FOR AC 8139. (LP# 1804346; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026091105089](https://openairdocs.org/sdr/DALA2026091105089.md): Support · corroded · Sep 9, 2026 · N139DU · Airbus BD5001A10
  > CORROSION ON WTB FAIRING SUPPORT STRUCTURE FROM FRAME 46R TO FRAME 46R+4" AT STR 35R.. ACCOMPLISHED ER/A# 636699-14 REV-ORIGINAL. ASSOCIATED ER/A 14-636699 ADDED FOR AC 8139. (LP# 1804322; AIRCRAFT WAS GROUNDED)
- [SDR HNAA2026100100935](https://openairdocs.org/sdr/HNAA2026100100935.md): Angle · cracked · Sep 8, 2026 · N650AE · Emb EMB145LR
  > RIGHT FR48, WING STUB, WING TO BODY, ANGLE CRACKED. R & R ANGLE IAW SRM 51-40-02
- [SDR 1Q2R2026092020076](https://openairdocs.org/sdr/1Q2R2026092020076.md): Diaphragm · cracked · Sep 8, 2026 · N706PS · Cndair CL6002C10
  > LEFT LOWER WING-TO-FUSELAGE FAIRING AT FS909.00 DIAPHRAGM IS CRACKED 1.60" FROM LOWER T/E. PERFORMED PERMANENT REPAIR IN ACCORDANCE WITH RFTS-130787 REV. 0, DATED SEPTEMBER 08, 2026, AND MHI RJ REO 670-53-82-478 REV. -A, DATED NOVEMBER 12, 2014.
- [SDR DALA2026091605181](https://openairdocs.org/sdr/DALA2026091605181.md): Longeron · corroded · Sep 8, 2026 · N301DU · Airbus BD5001A11
  > ER/A 636601-14 CORROSION REPAIR TO WING TO BODY FAIRING LH LONGERON BETWEEN FR 40 TO FR 48 REQUIRES FOLLOW ON ACTION. ACCOMPLISH 636601-14 SECT II REP INSPECTION WITHIN EVERY 1000 FLIGHT HOURS FROM SECT I ACCOMPLISHMENT. ACCOMPLISH SECT III PERMANENT REPAIR WI
- [SDR EE4Y2026090824946](https://openairdocs.org/sdr/EE4Y2026090824946.md): Rib · cracked · Sep 8, 2026 · N306JB · Emb ERJ190100IGW
  > DURING THE INSPECTION, WAS FOUND IN THE LT WING TO FUSELAGE FAIRING AT FR52 THE RIB CRACKED, DUE TO THIS, WAS PERFORMED A PERMANENT REPAIR IAW ETD2016-190-054721 DTD JUN 10 2016 AND DOCUMENTED UNDER COOPESA EO # COO-EO-2026-24815-R00 DTD AUG 03 2026. JOB A1Q35
- [SDR 1Q2R2026092220197](https://openairdocs.org/sdr/1Q2R2026092220197.md): Diaphragm · cracked · Sep 7, 2026 · N528EG · Cndair CL6002C10
  > LEFT LOWER WING-TO-FUSELAGE FAIRING AT BS 909 DIAPHRAGM IS CRACKED, 1.60" FROM LOWER T/E. PERFORMED PERMANENT REPAIR IAW RFTS-130820 REV. 0, AND REO 670-53-82-478 REV. -A.
- [SDR IPXA2026091123185](https://openairdocs.org/sdr/IPXA2026091123185.md): Fairing · eroded · Sep 7, 2026 · N623UP · Boeing 7478F
  > ERODED PANEL, WING TO BODY FAIRING PANEL 192AR FWD EDGE. I.A.W. 747-8F SRM 53-00-70-2R-1 REFER TO SRM 51-70-04-2R-1 AND SRM 51-80-03-0G-0 REV. 49 PERFORM REPAIR AS BELOW STEP:1.1 REMOVE THE EROSION MATERIALS AND CLEAN.1.2 MEASURE THE DAMAGE AREA ( L: 7", W
- [SDR IPXA2026091223189](https://openairdocs.org/sdr/IPXA2026091223189.md): Panel · eroded · Sep 7, 2026 · N623UP · Boeing 7478F
  > EROSION - PANEL, WING TO BODY FAIRING PANEL 192AGR FWD EDGE. IAW SRM 53-00-70-2R-1 REFER TO SRM 51-70-05-2R-1 AND SRM 51-80-03-0G-0 REV. 49 PERFORM REPAIR AS BELOW STEP:1.1 REMOVE THE EROSION MATERIALS AND CLEAN. 1.2 MEASURE THE DAMAGE AREA ( L: 14", W: 1.2
- [SDR IPXA2026091223226](https://openairdocs.org/sdr/IPXA2026091223226.md): Panel · eroded · Sep 7, 2026 · N623UP · Boeing 7478F
  > ERODED PANEL, WING TO BODY FAIRING PANEL 191FFL FWD EDGE. I.A.W. 747-8F SRM 53-00-70-2R-1 REFER TO SRM 51-70-05-2R-1 AND SRM 51-80-03-0G-0 REV. 49 PERFORM REPAIR AS BELOW STEP:1.1 REMOVE THE EROSION MATERIALS AND CLEAN.1.2 MEASURE THE DAMAGE AREA ( L: 5.5",
- [SDR SWAA2026101461993](https://openairdocs.org/sdr/SWAA2026101461993.md): Access Panel · delaminated · Sep 4, 2026 · N8656B · Boeing 7378H4
  > DELAMINATED ACCESS PANEL 193CL, WING TO BODY FAIRING. REPAIRED THE W-B FAIRING ACCESS PANEL 193CL IAW SRM 51-70-05-2R-10, REPAIR 10.
- [SDR REXA2026102001966](https://openairdocs.org/sdr/REXA2026102001966.md): Diaphragm · cracked · Sep 3, 2026 · N479PX · Cndair CL6002D24
  > CRACKED DIAPHRAGMA, FWD SUPPORT STRUCTURE, AFT WING-TO-FUSELAGE, BS 849, LBL 17.63. THE DIAPHRAGMA FWD SUPPORT STRUCTURE, AFT WING-TO-FUSELAGE WAS REPAIRED IAW EA CRJ953-23208, REV IR.
- [SDR CALA2026090319212](https://openairdocs.org/sdr/CALA2026090319212.md): Panel · damaged · Sep 2, 2026 · N831UA · Airbus A319131
  > FAIRING PANEL 192DT RAMP DISCOVERED PANEL 192 DT DAMAGED ON WALK AROUND. NO LARGE PORTIONS OF PANEL DEPARTED AIRCRAFT. PANEL WAS TORN FROM LEADING EDGE AROUND 2 FT TOWARD THE BACK.
- [SDR UIEA2026082700808](https://openairdocs.org/sdr/UIEA2026082700808.md): Support Frame · broken · Sep 1, 2026 · N489MC · Boeing 747412F
  > BS 1480, RT BLG WW FIXED FAIRING SUPPORT FRAME FOUND BROKEN. THE SUPPORT FRAME WAS REPAIRED IAW RI-53-60-18459, REV A. NO FURTHER DEFECTS NOTED.
- [SDR SWAA2026100589554](https://openairdocs.org/sdr/SWAA2026100589554.md): Access Panel · delaminated · Aug 30, 2026 · N8712L · Boeing 7378
  > DELAMINATED WING TO BODY FAIRING ACCESS PANEL 193CL. REPAIRED THE ACCESS PANEL 193CL IAW SRM 51-70-05-2R-10, REPAIR 10.
- [SDR DALA2026083104911](https://openairdocs.org/sdr/DALA2026083104911.md): Switch · loose · Aug 30, 2026 · N928AT · Boeing 717200
  > TAIL CONE EXIT TOGGLE SWITCH/LATCH LOOSE. CORRECTIVE ACTION: RESECURED AND ADJUSTED HARDWARE PER B717 AMM 52-22, NO OHTER FAULTS NOTED A/C OK TO CONT IN SVC. (9488400) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026090104932](https://openairdocs.org/sdr/DALA2026090104932.md): Frame · corroded · Aug 29, 2026 · N301DU · Airbus BD5001A11
  > CORROSION ON AFT WING TO BODY FAIRING FRAME AT MULTIPLE LOWER PANEL FASTENER HOLES. REMOVED AND REPLACED THE FAIRING FRAME IAW 51-77-00. (LP# 1783796; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026090104931](https://openairdocs.org/sdr/DALA2026090104931.md): Frame · corroded · Aug 29, 2026 · N301DU · Airbus BD5001A11
  > CORROSION ON AFT WING TO BODY FAIRING FRAME AT MULTIPLE LOWER PANEL FASTENER HOLES. REMOVED AND REPLACED THE FAIRING FRAME IAW 51-77-00. (LP# 1783791; AIRCRAFT WAS GROUNDED)
- [SDR CALA2026090119118](https://openairdocs.org/sdr/CALA2026090119118.md): Support Frame · cracked · Aug 29, 2026 · N23707 · Boeing 737724
  > LEFT WING TO BODY FAIRING SUPPORT FRAME CRACKED. REPAIRED THE WING TO BODY SUPPORT FRAME IAW REO G26037 AND EC/RA 5360-02207, REV -.
- [SDR HNAA2026100500947](https://openairdocs.org/sdr/HNAA2026100500947.md): Angle · cracked · Aug 27, 2026 · N653AE · Emb EMB145LR
  > RIGHT WING STUB, FUSE TO WING BOX ANGLE CRACKED AT FR 46. R & R ANGLE IAW SRM 51-40-02
- [SDR R61A2026092600273](https://openairdocs.org/sdr/R61A2026092600273.md): Strap · corroded · Aug 27, 2026 · N211YX · Emb ERJ170200LR
  > DURING HEAVY CHECK, MAINTENANCE FOUND AFT WTF FAIRING ATTACHMENT STRAP BETWEEN FR 73- 75, STR 23R - 29R CORRODED. THE ATTACHMENT STRAP WAS REMOVED AND REPLACED IAW SRM 51-43-04 AND 51-41-02.
- [SDR R61A2026092600272](https://openairdocs.org/sdr/R61A2026092600272.md): Strap · corroded · Aug 27, 2026 · N211YX · Emb ERJ170200LR
  > DURING HEAVY CHECK MAINTENANCE FOUND AFT WTF FAIRING ATTACHMENT STRAP BETWEEN FR 73- 75, STR 23L - 29L CORRODED. WTBF FAIRING ATTACHMENT STRAP WAS REMOVED AND REPLACED IAW SRM 51-43-04 AND 51-41-02.
- [SDR R61A2026092600271](https://openairdocs.org/sdr/R61A2026092600271.md): Support · corroded · Aug 27, 2026 · N211YX · Emb ERJ170200LR
  > DURING HEAVY CHECK MAINTENANCE FOUND WTB FAIRING RIB LT & RT SUPPORT CORRODED AT CFII FR54. THE WTB FAIRING RIB SUPPORT WAS REPLACED IAW SRM 51-41-02, AND 51-42-02.
- [SDR R61A2026092600262](https://openairdocs.org/sdr/R61A2026092600262.md): Strap · corroded · Aug 26, 2026 · N211YX · Emb ERJ170200LR
  > DURING HEAVY CHECK, MAINTENANCE FOUND CORRODED FWD WTB FAIRING TO FUSELAGE STRAP FOUND ON CFII AT FR 27-28, STR 24R-28L. THE FWD WTB FAIRING TO FUSELAGE STRAP WAS REPLACED IAW SRM 51-42-02, SRM 51-43-04 AND SRM 51-41-02.
- [SDR SWAA2026090169727](https://openairdocs.org/sdr/SWAA2026090169727.md): Panel · delaminated · Aug 25, 2026 · N8546V · Boeing 7378H4
  > PANEL 193CL LEADING EDGE HAS AREA OF EROSION AND DELAMINATION. R & R PANEL 193CL PER AMM 53-51-21.
- [SDR DALA2026082604830](https://openairdocs.org/sdr/DALA2026082604830.md): Radome · damaged · Aug 24, 2026 · N314NB · Airbus A319114
  > BIRD STRIKE ON LANDING ROLL NO ABNORMAL ENGINE INDICATIONS OR ODOR. C/W BIRD STRIKE INSPECTION, REMAINS REMOVED IAW AMM 05-51-14, FOUND PERFORATION DAMAGE TO RADOME APPLIED REPAIR IAW AMM 53-15-11. ACFT OK FOR SERVICE. (LP: 9318514, AIRCRAFT WAS GROUNDED)
- [SDR SWAA2026092192325](https://openairdocs.org/sdr/SWAA2026092192325.md): Rub Strip · gouged · Aug 20, 2026 · N266WN · Boeing 7377H4
  > GOUGED RUB STRIP ON THE BODY FAIRING LOWER ANGLE, BS 540 + 10 INCHES AND RBL 41. REPAIRED THE RUB STRIP IAW SRM 57-10-13-2R-3.

Next page: https://openairdocs.org/jasc/5350/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 = '5350'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/jasc/5350/reports

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