# Service difficulty reports: JASC 5513

A list on [JASC 5513](https://openairdocs.org/jasc/5513.md).

Reports filed under 5513 · Horizontal Stabilizer, Tab Structure, newest first.

Page 1 of 2 · 97 reports

- [SDR SWAA2026091494497](https://openairdocs.org/sdr/SWAA2026091494497.md): Blade · cracked · Aug 24, 2026 · N204WN · Boeing 7377H4
  > CRACK BLADE ACCESS PANEL 333AT ON LT HORIZONTAL STAB. REPLACED BLADE AND FASTENER FOR ACCESS PANEL 333AT IAW SRM 51-40-02.
- [SDR JR2R202410120002](https://openairdocs.org/sdr/JR2R202410120002.md): Stringer · damaged · Oct 12, 2024 · N87306 · Emb ERJ170200LR
  > RH HORIZ STRINGERS HAVE DRILL MARKS
- [SDR SWIA2023042700010](https://openairdocs.org/sdr/SWIA2023042700010.md): Unknown · damaged · Apr 17, 2023 · N140SY · Emb ERJ170200LR
  > RH HORIZONTAL STABILIZER UPPER SKIN HAS DAMAGE AT MULTIPLE AREAS AS MARKED. PN 170-62726-016 (C-CHECK RO 4/26/2023) PERFORMED REPAIRS ON NUMEROUS HOLES ON RH HORIZINTAL UPPER SKIN. REF ETD2023-170-009838 REV C. ADDITIONAL WEIGHT COMES OUT TO 304.2G THIS
- [SDR SWAA2023041024041](https://openairdocs.org/sdr/SWAA2023041024041.md): Seal · cracked · Apr 6, 2023 · N468WN · Boeing 7377H4
  > -LEFT HORIZONTAL STAB FWD UPPER SLIDING SEAL CRACKED.<[01] R&R LEFT HORIZONTAL STAB FWD UPPER SLIDING SEAL REF AMM 53-31-31.;[02] R&R LEFT HORIZONTAL STAB FWD UPPER SLIDING SEAL REF AMM 53-31-31.
- [SDR 7C7A2023022000014](https://openairdocs.org/sdr/7C7A2023022000014.md): Tab · cracked · Feb 20, 2023 · N887EA · Dhav DHC8106
  > IN PROCESS OF REPAIRIND DENTED SKIN REAR SPAR OF ELEVATOR TRIM TAB FOUND CRACKED
- [SDR SWIA20230206](https://openairdocs.org/sdr/SWIA20230206.md): Not Reported · dented · Feb 6, 2023 · N770SK · Cndair CL6002C10
  > LEFT FUSELAGE STRUCTURE DENTED BY FS169.00 IN BETWEEN RADOME AND ACCESS PANEL 121 AL HAS BEEN EVALUATED AND FOUND TO BE OUT OF LIMITS PER SRM 53-00-31. REFERENCE FOR CP 26143452 FOR INITAL DISCREPANCY. THIS IS A "MAJOR REPAIR". FORM M-337 INITIATED. (FILED CLO
- [SDR GTIA2022072136545](https://openairdocs.org/sdr/GTIA2022072136545.md): None · corroded · Jul 18, 2022 · N536NK · Airbus A319132
  > CORROSION FOUND ON LH ELEVATOR / ACTUATOR FITTING 1 CAT B. RAF-01 2907357-02 OPENED. REF TI 5513-1602. SDR REQUIRED.-REPAIRED BORE OF HINGE FITTING #1 OF INBOARD ACTUATOR INBOARD LUG OF LH ELEVATOR IAW SRM 55-26-47-300-002. REPAIR INSPECTION THRESHOLD FROM COM
- [SDR GTIA2022072136544](https://openairdocs.org/sdr/GTIA2022072136544.md): None · corroded · Jul 18, 2022 · N536NK · Airbus A319132
  > CORROSION FOUND ON LH ELEVATOR FITTING 5 CAT B. RAF-01 2907359-02 OPENED. REF TI 5513-1602. SDR REQUIRED.-REPAIRED BORES OF HINGE FITTING #5 OF LH ELEVATOR IAW SRM 55-26-41-300-004. REPAIR INSPECTION THRESHOLD FROM COMPONENT FIRST FLIGHT IS 6 YEARS AND SUBSEQU
- [SDR GTIA2022072136543](https://openairdocs.org/sdr/GTIA2022072136543.md): None · corroded · Jul 18, 2022 · N536NK · Airbus A319132
  > CORROSION FOUND ON LH ELEVATOR FITTING 3 CAT B. RAF-01 2907359-01 OPENED. REF TI 5513-1602. SDR REQUIRED.-REPAIRED BORES OF HINGE FITTING #3 OF LH ELEVATOR IAW SRM 55-26-41-300-004. REPAIR INSPECTION THRESHOLD FROM COMPONENT FIRST FLIGHT IS 6 YEARS AND SUBSEQU
- [SDR GTIA2022072136542](https://openairdocs.org/sdr/GTIA2022072136542.md): None · corroded · Jul 18, 2022 · N536NK · Airbus A319132
  > CORROSION FOUND ON RH ELEVATOR FITTING 2 CAT B. RAF-01 2907361-01 OPENED. REF TI 5513-1602. SDR REQUIRED.-REPAIRED HINGE FITTING #2 OF RH ELEVATOR IAW SRM 55-26-41-300-004. REPAIR INSPECTION THRESHOLD FROM COMPONENT FIRST FLIGHT IS 6 YEARS, AND SUBSEQUENT INSP
- [SDR GTIA2022072136541](https://openairdocs.org/sdr/GTIA2022072136541.md): None · corroded · Jul 18, 2022 · N536NK · Airbus A319132
  > CORROSION FOUND ON RH ELEVATOR / ACTUATOR FITTING 2 CAT B. RAF-01 2907358-01 OPENED. SDR REQUIRED.-REPAIRED BORES OF HINGE FITTING #2 OF OUTBOARD ACTUATOR INBOARD LUG OF ELEVATOR RH SIDE IAW SRM 55-26-47-300-002. REPAIR INSPECTION THRESHOLD FROM COMPONENT FIRS
- [SDR GTIA2022072136540](https://openairdocs.org/sdr/GTIA2022072136540.md): None · corroded · Jul 18, 2022 · N536NK · Airbus A319132
  > CORROSION FOUND ON LH ELEVATOR FITTING 6 CAT B. RAF-01 2907360-01 OPENED. REF TI 5513-1602. SDR REQUIRED.-REPAIRED BORES OF HINGE FITTING #6 OF LH ELEVATOR IAW SRM 55-26-41-300-006. REPAIR INSPECTION THRESHOLD FROM COMPONENT FIRST FLIGHT IS 6 YEARS, AND SUBSEQ
- [SDR GTIA2022072136539](https://openairdocs.org/sdr/GTIA2022072136539.md): None · corroded · Jul 18, 2022 · N536NK · Airbus A319132
  > CORROSION FOUND ON LH ELEVATOR FITTING #2 CAT B. RAF-01 2907358-02 OPENED. REFR TI 5513-1602. SDR REQUIRED.-REPAIRED BORE OF HINGE FITTING #1 OF INBOARD ACTUATOR INBOARD LUG OF LH LH ELEVATOR IAW SRM 55-26-47-300-002. REPAIR INSPECTION THRESHOLD FROM COMPONENT
- [SDR GTIA2022072136538](https://openairdocs.org/sdr/GTIA2022072136538.md): None · corroded · Jul 18, 2022 · N536NK · Airbus A319132
  > CORROSION FOUND ON RH ELEVATOR FITTING 3 CAT B. RAF-01 2907361-02 OPENED. REF TI 5513-1602. SDR REQUIRED.-REPAIRED HINGE FITTING #3 OF RH ELEVATOR IAW SRM 55-26-300-004. REPAIR INSPECTION THRESHOLD FROM COMPONENT FIRST FLIGHT IS 6 YEARS, AND SUBSEQUENT INSPECT
- [SDR GTIA2022072136537](https://openairdocs.org/sdr/GTIA2022072136537.md): None · corroded · Jul 18, 2022 · N536NK · Airbus A319132
  > CORROSION FOUND ON RH ELEVATOR FITTING 5 CAT B. RAF-01 2907362-01 OPENED. REF TI 5513-1602. SDR REQUIRED.-REPAIRED HINGE FITTING #5 OF RH ELEVATOR IAW SRM 55-26-41-300-004. REPAIR INSPECTION THRESHOLD FROM COMPONENT FIRST FLIGHT IS 6 YEARS, AND SUBSEQUENT INSP
- [SDR GTIA2022072136536](https://openairdocs.org/sdr/GTIA2022072136536.md): None · corroded · Jul 18, 2022 · N536NK · Airbus A319132
  > CORROSION FOUND ON RH ELEVATOR FITTING 6 CAT B. RAF-01 2907362-02 OPENED. REF TI 5513-1602. SDR REQUIRED.-REPAIRED HINGE FITTING #6 OF RH ELEVATOR IAW SRM 55-26-41-300-006. REPAIR INSPECTION THRESHOLD FROM COMPONENT FIRST FLIGHT IS 6 YEARS, AND SUBSEQUENT INSP
- [SDR GTIA2022072136535](https://openairdocs.org/sdr/GTIA2022072136535.md): None · corroded · Jul 18, 2022 · N536NK · Airbus A319132
  > CORROSION FOUND ON RH ELEVATOR FITTING 1 CAT B. RAF-01 2907360-02 OPENED. REF TI 5513-1602. SDR REQUIRED.-REPAIRED HINGE FITTING #1 OF RH ELEVATOR IAW SRM 55-26-41-300-004. REPAIR INSPECTION THRESHOLD FROM COMPONENT FIRST FLIGHT IS 6 YEARS, AND SUBSEQUENT INSP
- [SDR AALA202207054259](https://openairdocs.org/sdr/AALA202207054259.md): Bushing · excess play · Jul 3, 2022 · N921NN · Boeing 737
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY, LEFT HAND HORIZONTAL STABILIZER ELEVATOR TAB, HINGE 6. REPLACED HINGE BUSHINGS PER AMM 27-31-31-000-801 AND AMM 27-31-31-400-801. ACCOMPLISHED SATISFACTORY FREE PLAY CHECK PER AMM 27-31-32-200-805.
- [SDR AALA202207054025](https://openairdocs.org/sdr/AALA202207054025.md): Bushing · excess play · Jul 3, 2022 · N921NN · Boeing 737
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY, LEFT HAND HORIZONTAL STABILIZER ELEVATOR TAB, HINGE 5. REPLACED HINGE BUSHINGS PER AMM 27-31-31-000-801 AND AMM 27-31-31-400-801. ACCOMPLISHED SATISFACTORY FREE PLAY CHECK PER AMM 27-31-32-200-805.
- [SDR UIEA2022042800413](https://openairdocs.org/sdr/UIEA2022042800413.md): None · none · Apr 30, 2022 · N477MC · Boeing 74747UF
  > CORROSION DAMAGES ON RH HST CENTER SECTION UPPER SKIN TOP SURFACE BETWEEN STAB STA 143.6 AND 172.4, STRINGER 3 TO 12(<P>1) REMOVE THE AFFECTED FASTENERS IAW SRM 51.40.02 REV 94 2) BLENDED OUT THE DAMAGE AREA IAW SRM 51-10-02 REV 94 3) PFM NOT INSP REFER TO JOB
- [SDR AALA202202231340](https://openairdocs.org/sdr/AALA202202231340.md): Attach Fitting · gouged · Feb 5, 2022 · N930AN · Boeing 737*
  > AIRCRAFT IN BASE MAINTENANCE: GOUGE IN OUTBD ATTACH FITTING OF LH ELEVATOR CONTROL TAB MECHANISM FROM PREVIOUSLY INSTALLED FASTENER AT STA 36.4, MEASURING D=0.012 IN. REPLACED FITTING WITH NEW IAW B737-NG SRM 55-20-90-1A.
- [SDR SWIA202165007](https://openairdocs.org/sdr/SWIA202165007.md): None · damaged · Dec 29, 2021 · N854AS · Cndair CL6002B19
  > TOP PLATE FOR 1EA NUTPLATE ON THE RIGHT HORIZONTAL TIP HAS DAMAGE (MARKED) (C-CHECK RO 3/14/2022) REPAIRED TOP PLATE ON RIGHTHAND HORIZONTAL TIP IAW REO 601R-55-11-712 REV -- DATE 2022-02-01 STEPS. 1-9. (SEE CONTINUATION SHEET FOR FURTHER DETAILS) COMPLI
- [SDR SWIA202165005](https://openairdocs.org/sdr/SWIA202165005.md): None · corroded · Dec 29, 2021 · N854AS · Cndair CL6002B19
  > RH HORIZONAL STAB LE ERODED. (C-CHECK RO 3/14/2022) REMOVED EROSION ON RH HORIZONAL STAB LE, REF. CRJ200 SRM 51-12-00 / COMPLIED WITH REO 601R-55-12-716 REV -- DATE 2022-01-20
- [SDR SWIA202163729](https://openairdocs.org/sdr/SWIA202163729.md): None · mislocated · Dec 5, 2021 · N207PS · Cndair CL6002B19
  > L/H HORZONAL STAB TIP PANEL HAS MISLOCATED NUTPLATE ON INBOARD EDGE, THIRD NUTPLATE FWD OF TRAILING EDGE OF STAB TIP. (C-CHECK RO 1/5/2022) REMOVED AND REPLACED RIB AND SPLICE WITH NEW FABRICATED PN: 600-23079-S0101 RIB AND PN: 600-23037-22 SPLICE IAW R
- [SDR A6WA202111187973](https://openairdocs.org/sdr/A6WA202111187973.md): None · corroded · Nov 13, 2021 · N426AW · Cndair CL6002B19
  > PAX DOOR FWD ANCHO FITTING PLATE P/N600-38061-11 WAS FOUND CORRODED. THE EXPANSION CAUSED THE PAX DOOR FWD ANCHOR FITTING TO CRACK. ***AIRCRAFT REMOVED FROM SERVICE*** R&R PAX DOOR FWD ANCHOR PLATE AND ALL ATTACHING HARDWARE, FWD PAX DOOR SWIVEL CABLE END,
- [SDR SWIA202161978](https://openairdocs.org/sdr/SWIA202161978.md): None · damaged · Oct 30, 2021 · N472CA · Cndair CL6002B19
  > FORM M-337 REQUIRED DUE TO DAMAGE ON RH HORIZONTAL STABILIZER IAW REO 601R-55-11-701 (FILED CLOSED) COMPLIED WITH M-337
- [SDR SWIA202161977](https://openairdocs.org/sdr/SWIA202161977.md): Doubler · damaged · Oct 30, 2021 · N472CA · Cndair CL6002B19
  > INSPECTED R/H HORIZONTAL STABILATOR AND FOUND DAMAGE ON FRAME 9 (3/4 INCH HOLES WHERE TWO NUT PLATES BLEW OUT), SKIN IN RIGHT AFT CORNER (1/2 INCH HOLE) AND DAMAGE ON AFT SPAR (3/4 INCH HOLES WHERE ONE NUT PLATE BLEW OUT). (FILED CLOSED) REPAIRED DAMAGE
- [SDR A6WA202110297941](https://openairdocs.org/sdr/A6WA202110297941.md): None · none · Aug 27, 2021 · N439AW · Cndair CL6002B19
  > H/STAB PCU ACCESS PANEL #332AB (P/N: 601R23052-11) HAS 3EACH DAMAGED HOLES. DIMENSIONS: HOLE #1:.195" X.258"; HOLE #2:.310" X.220"; HOLE #3:.195" DIA ***AIRCRAFT REMOVED FROM SERVICE*** REAMED HOLES TO FOLLOWING DIMENSIONS: HOLE #1:.3685"; HOLE #2:.37
- [SDR SWIA202161700](https://openairdocs.org/sdr/SWIA202161700.md): None · dented · Aug 10, 2021 · N946SW · Cndair CL6002B19
  > * R/H HORIZONTAL STABILIZER UPPER SKIN HAS A DENT AT APPROX. HSS100, MARKED. (C-CHECK RO 10/8/2021) PERFORMED CUT OF R/H HORIZONTAL STABILIZER UPPER SKIN AT BETWEEN RIB 7 & RIB 6 AND STGR2 & STGR3 REF CRJ200 SRM 55-11-31. COMPLIED WITH 51-900-1003-SKY
- [SDR MASA20200727056](https://openairdocs.org/sdr/MASA20200727056.md): Tab · damaged · Jul 27, 2020 · N927LR · Cndair CL6002D24
  > (C-CHECK) HSTAB PIVOT FITTING LHS/RHS ANTI-ROTATION TABS DAMAGED. REPAIRED I/A/W SB 670BA-55-012 & 670BA-55-013.
- [SDR O2GA2020052801](https://openairdocs.org/sdr/O2GA2020052801.md): Panel · missing · May 16, 2020 · N885UP · Beech B300
  > FROZEN STABILIZER TRIM FROZEN NOTICED AT TOP OF DESCENT. TRIM UNFROZE AT LOWER ALTITUDES. DIVERTED TO KVNY. LANDING WAS UNEVENTFUL. MAINTENANCE FOUND THE LEFT TRIM TAB ACTUATOR PANEL MISSING FROM THE TOP OF THE STAB. STAB TRIM ACTUATOR WAS LUBRICATED, PANEL WA
- [SDR BIER2020042700000](https://openairdocs.org/sdr/BIER2020042700000.md): Balance Weight · rusted · Apr 27, 2020 · N8187H · Piper PA44180T
  > DURING ANNUAL INSPECTION BY CRS # BIER466C, FOUND BALANCE WEIGHT ASSEMBLY P/N 38398-005 RUSTED THROUGH. RECEIVED NEW PIPER PART NUMBER 38398-005 AS REPLACEMENT. THE NEW ASSEMBLY COMES CONSIDERABLY OVER-SIZED. ADDRESS THE ISSUE WITH PIPER DSA TOM PENTECOST (DSA
- [SDR DALA2017041302974](https://openairdocs.org/sdr/DALA2017041302974.md): Tab · dented · Apr 12, 2017 · N917DL · Doug MD88
  > HORIZONTAL STABILIZER DENTED ON THE LT & RT ANTI FLOAT TAB UPPER SURFACE. THE ANTI FLOAT TABS WERE REPAIRED IAW SRM 55-04 P. 3.
- [SDR DALA2017040702796](https://openairdocs.org/sdr/DALA2017040702796.md): Skin · delaminated · Apr 6, 2017 · N917DL · Doug MD88
  > HORIZONTAL STABILIZER, DELAMINATION ON LT ANTI-FLOAT TAB UPPER/LOWER SURFACE. ANTI-FLOAT TAB WAS REPAIRED PER SRM 55-04 P 3.
- [SDR DALA2017032302332](https://openairdocs.org/sdr/DALA2017032302332.md): Tab · dented · Mar 22, 2017 · N912DE · Doug MD88
  > HORIZONTAL STABILIZER, DENT 1EA ON LT CONTROL TAB NEAR STA XHS= 68. LT CONTROL TAB NEAR STA XHS= 68 WAS REPAIRED PER SRM 55-04 FIGURE 2.
- [SDR DALA2017032302331](https://openairdocs.org/sdr/DALA2017032302331.md): Tab · damaged · Mar 22, 2017 · N912DE · Doug MD88
  > HORIZONTAL STABILIZER, PROTUBERANCE ON LT CONTROL TAB NEAR STA XHS= 86. LT CONTROL TAB NEAR STA XHS= 86 WAS REPAIRED PER SRM 55-04 PAR 3 CLASS A.
- [SDR WVER201503200003](https://openairdocs.org/sdr/WVER201503200003.md): Tab · gouged · Mar 20, 2015 · N925FJ · Cndair CL6002D24
  > RT HORIZONTAL ANTI-ROTATION TAB IS GOUGED FROM CONTACT WITH THE HORIZONTAL STABILIZER PIVOT PIN HARDWARE. REMOVED TAB IAW REO 670BA-55-012, PARTS A & B, REV D. NOTE: LT TAB HAS BEEN PREVIOUSLY REMOVED UNDER THE SAME REO.
- [SDR ASOA2014091611223](https://openairdocs.org/sdr/ASOA2014091611223.md): Tab · chafed · Sep 6, 2014 · N753EV · Cndair CL6002C10
  > CHAFE DAMAGE ON LT AND RT ANTI-ROTATION TABS OF THE HORIZONTAL STABILIZER. COMPLIED WITH EC/TC SB 670BA-55-012 01,02,03.
- [SDR DALA13034239205](https://openairdocs.org/sdr/DALA13034239205.md): Mechanism · gouged · Jul 9, 2013 · N905DA · Doug MD9030
  > RIGHT HORIZONTAL STABILIZER L/E FLOAT TAB MECHANISM GOUGED. REPAIRED IAW ERA 514984-14, REV O AND FINAL ERA 514894-14, REV O.
- [SDR DALA13034249205](https://openairdocs.org/sdr/DALA13034249205.md): Bracket · gouged · Jul 7, 2013 · N905DA · Doug MD9030
  > LEFT HORIZONTAL STABILIZER FLOAT TAB BRACKET GOUGED. REPAIRED IAW ERA 514894-14, REV O.
- [SDR A6WA201141102](https://openairdocs.org/sdr/A6WA201141102.md): Fitting · damaged · Nov 3, 2011 · N470ZW · Cndair CL6002B19
  > HORZONTAL STAB PIVOT FITTING DAMAGED ON LT INBD FWD FACE. BLENDED DAMAGED AREA NDT INSPECTION FLAP PEENED, ALODINED, PRIMED IAW REO 601R-55-11-392.
- [SDR A6WA201141101](https://openairdocs.org/sdr/A6WA201141101.md): Pivot · damaged · Nov 3, 2011 · N470ZW · Cndair CL6002B19
  > HORZONTAL STAB TRIM ACTUATOR PIVOT STRUCTURE DAMAGED ON LT OTBD FACE. BLENDED DAMAGED AREA NDT INSPECTION PRIMED IAW REO 601R-55-31-220.
- [SDR DALA1119700916](https://openairdocs.org/sdr/DALA1119700916.md): Skin · dented · Mar 17, 2011 · N916DL · Doug MD88
  > DURING HMV A DENT WAS FOUND ON UPPER SKIN OF RT GEARED TAB. GEARED TAB WAS REPAIRED IAW SRM 55-04 PAR 3A.
- [SDR DLM88091321](https://openairdocs.org/sdr/DLM88091321.md): Tab · corroded · Aug 12, 2009 · N910DL · Doug MD88
  > DURING SHOP VISIT THE SUBJECT HORIZONTAL STABILIZER ELEVATOR ANTI-FLOAT TAB WAS FOUND WITH CORROSION. REPAIRED PER ERA 474926-14.
- [SDR QXEA2009051100321](https://openairdocs.org/sdr/QXEA2009051100321.md): Tab · damaged · May 8, 2009 · N600QX · Cndair CL6002C10
  > DAMAGED LT AND RT ANTI ROTATION TABS OF THE HORIZ STAB PIVOT FITTING P/N AV670-23120, REMOVED PANELS 326CL AND 326CR. REMOVED HORIZ STAB PIVOT BOLT INNER PIN AND LT OUTER PIN, TRIMMED CHAFED LT LOCK TAB IAW TC REO 670-55-11-099 GENERAL NOTES 1-3. COMPLIED
- [SDR SWAA060864](https://openairdocs.org/sdr/SWAA060864.md): Tab · cracked · Mar 16, 2006 · N305SW · Boeing 7373H4
  > DURING SCHEDULED C4 CHECK, FOUND RT ELEVATOR TAB CRACKED AT NR 2 HINGE CUTOUT. REMOVED AND REPLACED TAB PER MM.
- [SDR 05FDEA00499](https://openairdocs.org/sdr/05FDEA00499.md): Splice · corroded · Mar 11, 2005 · N481FE · Boeing 727200
  > CORROSION ON STRINGER SPLICE AT BS 678 STRINGER 28L. INSTALLED NEW STRINGER SPLICE AT BS 678, STR 28L IAW SRM 51-30-2 & SRM 51-10-2.
- [SDR WRLA2005031](https://openairdocs.org/sdr/WRLA2005031.md): Spar Cap · corroded · Feb 18, 2005 · N276 · Doug MD11F
  > DURING "C04" CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST LT BARREL NUT HOLE NR 36.
- [SDR WRLA2005032](https://openairdocs.org/sdr/WRLA2005032.md): Spar Cap · corroded · Feb 17, 2005 · N276 · Doug MD11F
  > DURING "C04" CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST RT BARREL NUT HOLE NR 01.
- [SDR WRLA2005037](https://openairdocs.org/sdr/WRLA2005037.md): Skin · corroded · Feb 11, 2005 · N276 · Doug MD11F
  > DURING "C04" CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST RT BARREL NUT HOLE NR 31.

Next page: https://openairdocs.org/jasc/5513/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 = '5513'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/jasc/5513/reports

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