# Service difficulty reports: JASC 5550

A list on [JASC 5550](https://openairdocs.org/jasc/5550.md).

Reports filed under 5550 · Empennage Flight Control Surfaces, Attach Fittings, newest first.

Page 1 of 2 · 66 reports

- [SDR DALA2024120411445](https://openairdocs.org/sdr/DALA2024120411445.md): Bushing · corroded · Nov 27, 2024 · N336NB · Airbus A319114
  > SHIP 3136 CORROSION ON BUSH LOCATED AT ELEVATOR HINGE FITTING #3 I/B AND O/B LUG LH HORIZONTAL STABILIZER (2 EA). CORRECTIVE ACTION: REPLACED BUSHINGS (2 EA) ON HINGE #3 AT L/H ELEVATOR AS PER A319 SRM 55-26-41-300-004. (0681477)
- [SDR DALA2024120411444](https://openairdocs.org/sdr/DALA2024120411444.md): Bushing · corroded · Nov 27, 2024 · N336NB · Airbus A319114
  > SHIP 3136 CORROSION ON BUSH LOCATED AT ELEVATOR HINGE FITTING #1 I/B AND O/B LUG LH HORIZONTAL STABILIZER (2 EA). CORRECTIVE ACTION: REPLACED BUSHINGS (2 EA) ON HINGE #1 AT L/H ELEVATOR AS PER A319 SRM 55-26-41-300-004. (0681458)
- [SDR VNAA202304270015](https://openairdocs.org/sdr/VNAA202304270015.md): Hinge Fitting · corroded · Mar 16, 2023 · N619NN · Cndair CL6002D24
  > CORROSION ON LOWER RUDDER HINGE AT REAR SPAR OF VERTICAL STABILIZER
- [SDR IPXA2022030479714](https://openairdocs.org/sdr/IPXA2022030479714.md): Fitting · none · Feb 23, 2022 · N278UP · Doug MD11F
  > INSPECTION TYPE:1CLH HORIZONTAL STAB ELEVATOR #3 ACTUATOR HINGE SUPPORT FITTING IS CHAFE AT STA XE=122.REPAIRED CHAFED HINGE SUPPORT FITTING IAW VT-SAA EA 011-5510-01-A9501 REV I/R AND UPS EO MD11-5550-83032-A (MINOR).
- [SDR DALA2021121607800](https://openairdocs.org/sdr/DALA2021121607800.md): None · none · Dec 13, 2021 · N357NW · Airbus A320212
  > SHIP 3257 CORROSION ON BUSHING (1EA) ON OUTBOARD ACTUATOR FITTING INBOARD LUG RH ELEVATOR. CORRECTIVE ACTION: REPAIRED BORE AND REPLACED BUSHING (1EA) OF IB LUG ON OB ACTUATOR FITTING ON RH ELEVATOR AS PER A320 SRM 55-26-47. (2050657)
- [SDR DALA2021121607799](https://openairdocs.org/sdr/DALA2021121607799.md): None · none · Dec 13, 2021 · N357NW · Airbus A320212
  > SHIP 3257 CORROSION ATTACH FITTING ELEVATOR ACTUATOR INBOARD SIDE INBOARD ACTUATOR ON RH HORIZONTAL STABILIZER. CORRECTIVE ACTION: REPAIRED BORE AND REPLACED BUSHING (1EA) OF IB LUG ON IB ACTUATOR FITTING OF RH ELEVATOR AS PER A320 SRM 55-26-47. (2050646)
- [SDR DALA2021121607798](https://openairdocs.org/sdr/DALA2021121607798.md): None · none · Dec 13, 2021 · N357NW · Airbus A320212
  > SHIP 3257 CORROSION ATTACH FITTING ELEVATOR ACTUATOR OUTBOARD ACTUATOR INBOARD SIDE ON LH HORIZONTAL STABILIZER. CORRECTIVE ACTION: REPAIRED BORE AND REPLACED BUSHING (1EA) OF I/B LUG ON OB ACTUATOR FITTING OF LH ELEVATOR AS PER A320 SRM 55-26-47. (2050630)
- [SDR FDEA201205181858](https://openairdocs.org/sdr/FDEA201205181858.md): Intercostal · cracked · May 18, 2012 · N612FE · Doug MD11F
  > NR 2 ENGINE AIR INTAKE INSIDE PANEL 363PL FOUND WIRE CUT-OUT INTERCOSTAL CRACKED. CARRIED OUT REPAIR IAW SRM 55-30-02, FIG 201. REPAIR 2 REV 49. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.
- [SDR IPXA2M73978](https://openairdocs.org/sdr/IPXA2M73978.md): Fitting · worn · May 10, 2012 · N290UP · Doug MD11F
  > INSPECTION TYPE: 4C, ONE SHEARED FASTENER ON FWD SIDE LOWER FASTENER OF THE NR 4 BANJO FITTING LT SIDE. REPAIRED VERT STAB AFT SPAR NR 4 BANJO FITTING LT SIDE REF EO MD11-5530-46641-A APPX C AND E.
- [SDR IPXA2M73977](https://openairdocs.org/sdr/IPXA2M73977.md): Fitting · worn · May 10, 2012 · N290UP · Doug MD11F
  > INSPECTION TYPE: 4C, ONE LOOSE FASTENER ON FWD SIDE LOWER FASTENER OF THE NR 4 BANJO FITTING RT SIDE. REPAIRED VERTICAL STAB AFT SPAR NR 4 BANJO FITTING RT SIDE, REF EO MD11-5530-46641-A APPX B AND D.
- [SDR C2XA09SH177](https://openairdocs.org/sdr/C2XA09SH177.md): Bracket · damaged · Jun 29, 2009 · N12540 · Emb EMB145LR
  > SHV - DURING C-CHECK, RUDDER 2 UPPER ATTACHMENT BRACKET HAS MIGRATED HAT BUSHING. REMOVED AND REPLACED RUDDER 2 UPPER HINGE BRACKET IAW SRM 55-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR 08FDEA04781](https://openairdocs.org/sdr/08FDEA04781.md): Support Fitting · cracked · Nov 7, 2008 · N593FE · Doug MD11F
  > EMPENNAGE, AFT FUSELAGE COMPARTMENT PRESSURE BULKHEAD UPPER AFT SURFACE QUANTITY 01 SUPPORT FITTING AT STATION 2007, X=-31.930 FOUND CRACKED.
- [SDR DLM90080204](https://openairdocs.org/sdr/DLM90080204.md): Plate · corroded · Feb 12, 2008 · N911DA · Doug MD9030
  > DURING HMV THE RT VERTICAL-TO-HORIZONTAL STABILIZER INBOARD AND OUTBOARD HINGE PLATES WERE FOUND WITH CORROSION IN THE BORES. A REPAIR WAS MADE AND APPROVED VIA FAA FORM 8100-9.
- [SDR IXXA07SMN271S](https://openairdocs.org/sdr/IXXA07SMN271S.md): Attach Angle · corroded · Nov 16, 2007 · N604BX · Doug DC873F
  > DURING ROUTINE C CHECK INSPECTION, FOUND FUSELAGE TO STABILIZER LEFT ATTACH ANGLE SHOWS CORROSION AT STATION 1754.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGES AREA. FABRICATED ANGLE. PERFORMED HEAT TREATMENT TO ANGLE. CLEANED, TREATED AND
- [SDR AMTA200600268](https://openairdocs.org/sdr/AMTA200600268.md): Bearing · corroded · Apr 3, 2006 · N163AT · Lkheed 10113853
  > DURING THE INSPECTION OF THE LT HORIZONTAL STABILIZER PIVOT BEARING INSPECTION, FOUND THE FOLLOWING ITEMS CORRODED, PIVOT BEARING, OUTER PIN, BEARING RETAINER NUT AND FITTING HOUSING. REPLACED THE PIVOT BEARING, OUTER PIN, BEARING RETAINER NUT AND FITTING HOU
- [SDR AMTA200600267](https://openairdocs.org/sdr/AMTA200600267.md): Bearing · corroded · Apr 3, 2006 · N163AT · Lkheed 10113853
  > DURING RT HORIZONTAL STAB PIVOT BEARING INSPECTION FOUND THE FOLLOWING ITEMS CORRODED. PIVOT BEARING, OUTER PIN, BEARING RETAINER NUT AND FITTING HOUSING. REPLACED PIVOT BEARING, OUTER PIN, BEARING RETAINER NUT AND FITTING HOUSING IAW AMM. FREEPLAY INSPECTI
- [SDR 06FDEA0807](https://openairdocs.org/sdr/06FDEA0807.md): Fitting · cracked · Feb 22, 2006 · N585FE · Doug MD11
  > EMPENNAGE, FORWARD UPPER DOG HOUSE ENTRANCE, CUT OUT EDGE FOUND CRACKED CORRECTIVE ACTION: SNRM NO.: N00958 - EMPENNAGE, FORWARD UPPER DOG HOUSE ENTRANCE, CUT OUT EDGE CRACKED AREA REPAIRED AS PER SRM 53-00-01 VOLUME I, FIGURE 5. REPAIR CLASSIFIED AS
- [SDR 06FDEA0370](https://openairdocs.org/sdr/06FDEA0370.md): Support Fitting · unknown · Jan 24, 2006 · N490FE · Boeing 727200
  > COMPLY WITH EO 7-5550-7-2302E SECTION 4B - RUDDER CENTER HINGE SUPPORT FITTING REPLACEMENT ON LOWER RUDDER. REPLACED HINGE SUPPORT FITTING PER E.O. 7-5550-7-2302E.
- [SDR MALA040625](https://openairdocs.org/sdr/MALA040625.md): Skin · dented · Oct 27, 2004 · N27XJ · Saab SF340A
  > DURING 4Y/2Y INSPECTION IN BNA, NOTED 7 DENTS IN LT UPPER STAB SKIN. FIVE ARE WITHIN LIMITS PER THE SRM & 2 WERE DELAMINATED AND REPAIRED PER EO S55017.
- [SDR 2004FA0000230](https://openairdocs.org/sdr/2004FA0000230.md): Sleeve · loose · Feb 20, 2004 · N922AF · Diamon DA20C1
  > THE SLEEVE ON THE RUDDER HINGE PIN CAME LOOSE FROM ITS LOCTITED POSITION ON THE PIN AND WORKED UP INTO THE CAVITY ABOVE THE BEARING ON THE FIN. RUDDER HAD CONSIDERABLE PLAY AT THE TOP.
- [SDR DL73S040175](https://openairdocs.org/sdr/DL73S040175.md): Attach Fitting · corroded · Feb 19, 2004 · N239WA · Boeing 737247
  > CORROSION WAS NOTED ON THE VERT STAB ATTACH LUGS, ON THE AFT FACE OF THE NR 6 FIN LUG. CORROSION REMOVED AND LUG REWORKED PER ERA 386225-14.
- [SDR DL73S040104](https://openairdocs.org/sdr/DL73S040104.md): Attach Fitting · corroded · Jan 28, 2004 · N319DL · Boeing 737232
  > NUMEROUS ATTACHMENT FITTING LUGS ON THE HORIZ STAB TO FUSELAGE JOINT REQUIRED MACHINING BEYOND PUBLISHED LIMITS IN ORDER TO REMOVE CORROSION. CORROSION WAS REMOVED AND LUGS REWORKED IAW ERA 386108-14AD.
- [SDR DL73S040103](https://openairdocs.org/sdr/DL73S040103.md): Fitting · corroded · Jan 28, 2004 · N242WA · Boeing 737247
  > DURING ACCOMPLISHMENT OF 03-085220-03 CORROSION WAS NOTED ON THE TWO VERT STAB FIN LUGS. ADDITIONALLY, TWO FUSELAGE CLEVIS LUGS WERE NOTED AS HAVING LUG THICKNESSES BELOW THAT ALLOWED BY 03-085220-03. CORROSION REMOVED AND LUGS/CLEVISES REWORKED PER ERA 3860
- [SDR N136FE0401](https://openairdocs.org/sdr/N136FE0401.md): Hinge · cracked · Jan 13, 2004 · N136 · Boeing 72725C
  > DURING SERVICE CHECK, FOUR CRACKS WERE FOUND ON THE NR 7 GROUND SPOILER SUPPORT HINGE. HINGE REPLACED WITH NEW PART. ALL HINGES INSPECTED FOR CRACKS, NO FAULTS FOUND.
- [SDR C2XA02TY191](https://openairdocs.org/sdr/C2XA02TY191.md): Bracket · gouged · Dec 29, 2002 · N17521 · Emb EMB135LR
  > TYS, During a scheduled inspection the left hand horizontal stab. actuator mounting bracket was found gouged. Maintenance removed and replaced the fitting I/A/W-EMB-135/145-SRM-51-40-02, CMP-51-21-04, 05 and 06. The repair was satisfactory and the aircraft wil
- [SDR CSA2002F00001](https://openairdocs.org/sdr/CSA2002F00001.md): Pivot Assy · cracked · Aug 27, 2002 · N995SB · Beech C99
  > USING VISABLE DYE PENTRANT INSPECTION, FOUND CRACKS IN STRUCTURAL WEBBING OF PIVOT POINT EXTENSIONS OF BOTH LEFT AND RIGHT HAND BRACKETS. CRACK ON LEFT BRACKET MEASURED APPROXIMATELY.5 INCHES. CRACK IN RIGHT BRACKET EXTENDED ENTIRE LENGTH OF WEB. TOTAL TIM
- [SDR USAA020206](https://openairdocs.org/sdr/USAA020206.md): Angle · cracked · Apr 17, 2002 · N373US · Boeing 7373B7
  > PIT - FOUND DRAG ANGLE CRACKED.25 INCH, SECT 48 DRAG ANGLE LIGHT SIDE 10 INCH BEHIND ATTACH LUG. REPAIRED FILLER AND STRAPS ON OUTSIDE AND INSIDE OF DRAG ANGLE PER TYPICAL REPAIR 53-80-03. (M)
- [SDR 2002FA0000377](https://openairdocs.org/sdr/2002FA0000377.md): Fitting · malfunctioned · Mar 2, 2002 · N5208C · Beech B35
  > LOOKED AT RUDDERVATORS MOVEMENT, THIS FITTING WAS MOVING, CALLED MANUFACTURER FOR INFORMATION ON THIS FITTING.
- [SDR CA011029008](https://openairdocs.org/sdr/CA011029008.md): Hinge · corroded · Sep 15, 2001 · Cessna 208
  > (CAN) WHILE PERFORMING AN ANNUAL INSPECTION ON THIS AIRCRAFT, EXCESSIVE MOVEMENT WAS NOTED FROM THE OUTBOARD AND CENTRE HINGE BEARINGS FOR THE R/H ELEVATOR. WHEN THE HINGE SUPPORTS WERE DISMANTLED TO REPLACE THE BEARINGS, CORROSION WAS FOUND ON BOTH HALVES OF
- [SDR USAASB01234](https://openairdocs.org/sdr/USAASB01234.md): Bolt · worn · Aug 18, 2001 · N351US · Boeing 737301
  > DCA - FLT 360 - ON CLIMB-OUT FROM DCA, EN ROUTE TO ROC, CREW FELT A RUMBLE/AIRFRAME VIBRATION THROUGHOUT THE CABIN. DUE TO PREVIOUS FILGHT SEGMENT EXPERIENCING THE SAME PROBLEM, FLIGHT RETURNED TO FIELD AT DCA. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EME
- [SDR CA011029012](https://openairdocs.org/sdr/CA011029012.md): Hinge · cracked · Aug 2, 2001 · Cessna 180J
  > (CAN) DURING 100 HOUR INSPECTION FOUND LT OUTBOARD ELEVATOR BEARING LOOSE. REMOVED LT ELEVATOR TO CHANGE BEARING. WITH ELEVATOR REMOVED, FOUND LT OUTBOARD HINGE ASSEMBLY TO BE CORRODED AND CRACKED WHERE BEARING IS INSTALLED.
- [SDR C2XA011A007](https://openairdocs.org/sdr/C2XA011A007.md): Bushing · corroded · Dec 30, 2000 · N15941 · Emb EMB145
  > IAH - DURING C-CHECK INSPECTION, THE RIGHT AND LEFT HORIZONTAL STABILIZER PLAIN BUSHINGS WERE FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PLAIN BUSHINGS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA011A006](https://openairdocs.org/sdr/C2XA011A006.md): Bushing · corroded · Dec 30, 2000 · N15941 · Emb EMB145
  > IAH - DURING C-CHECK INSPECTION, THE RIGHT AND LEFT HORIZONTAL STABILIZER FLANGED BUSHINGS WERE FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FLANGED BUSHINGS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR AALA20010062](https://openairdocs.org/sdr/AALA20010062.md): Hinge · corroded · Dec 19, 2000 · N3507A · Doug DC982
  > TUL - FOUND VERTICAL STABILIZER HINGE LUGS AND SPREADER HAVE PITTING, CORROSION IN AND AROUND BORES. INSTALLED NEW LUG PLATES AND SPREADER PER SRM 55-02 PAGE 68. (M)
- [SDR DL73K002264](https://openairdocs.org/sdr/DL73K002264.md): Fitting · corroded · Nov 20, 2000 · N310DA · Boeing 737232
  > THE VERTICAL STABILIZER ATTACHMENT LUGS WERE FOUND CORRODED AT HMV. ERA 396368-14 REMOVES CORROSION FROM THE BORES AND FACES OF THE LUGS AND REINSTALLS THE BUSHING AND SLEEVES.
- [SDR DL73K002258](https://openairdocs.org/sdr/DL73K002258.md): Fitting · corroded · Nov 20, 2000 · N310DA · Boeing 737232
  > CORROSION WAS REMOVED FROM THE HORIZONTAL STABILIZER ATTACH LUGS FROM THE BORE AND FACE. ERA 396375-14 REPAIRED THE AREA AT HMV.
- [SDR USAA002115](https://openairdocs.org/sdr/USAA002115.md): Clevis · corroded · Oct 24, 2000 · N518AU · Boeing 7373B7
  > PIT - FOUND CLEVIS LUG CORRODED.014 INCH DEEPEST AREA, RIGHT HORIZ STAB CENTER SECTION BOTTOM FORWARD CLEVIS BORE. REAMED, SPOTFACED AND CHAMFERED CLEVIS LUGS WITHIN LIMITS IN SRM 55-10-10. OVERSIZE BUSHINGS MANUFACTURED. (M)
- [SDR USAA002116](https://openairdocs.org/sdr/USAA002116.md): Clevis · corroded · Oct 24, 2000 · N518AU · Boeing 7373B7
  > PIT - FOUND CLEVIS LUG CORRODED.018 DEEPEST AREA, RIGHT HORIZONTAL STAB CENTER SECTION TOP FORWARD CLEVIS BORE. REAMED, SPOTFACED AND CHAMFERED CLEVIS LUGS WITHIN LIMITS IN SRM 55-10-10. OVERSIZE BUSHINGS MANUF. (M)
- [SDR USAA002117](https://openairdocs.org/sdr/USAA002117.md): Clevis · corroded · Oct 24, 2000 · N518AU · Boeing 7373B7
  > PIT - FOUND CLEVIS LUG CORRODED.004 INCH DEEPEST AREA, RIGHT HORIZ STAB CENTER SECTION TOP AFT CLEVIS BORE. REAMED, SPOTFACED AND CHAMFERED CLEVIS LUG WITHIN LIMITS IN SRM 55-10-10. OVERSIZE BUSHINGS MANUFACTURE. (M)
- [SDR DL73K002055](https://openairdocs.org/sdr/DL73K002055.md): Fitting · corroded · Oct 19, 2000 · N311DL · Boeing 737232
  > CORROSION WAS FOUND ON MULTIPLE LUGS ON THE VERTICAL STABILIZER ATTACHMENT LUGS AND FUSELAGE ATTACH LUGS. ALL CORROSION WAS REMOVED AND REPAIRED PER ERA 396259-14 AT HMV.
- [SDR C2XA00IA364](https://openairdocs.org/sdr/C2XA00IA364.md): Bushing · corroded · Oct 4, 2000 · N15932 · Emb EMB145
  > IAH-DURING C-CHECK INSPECTION, THE RIGHT HAND HORIZONTAL STABILIZER AFT ATTACHMENT INBOARD BUSHING WAS FOUND TO BE CORRODED AND PITTED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUSHING IN ACCORDANCE WITH EMB145 M/M 20-10-08, AND THE AIRCRAFT WAS APPROVED
- [SDR C2XA00IA363](https://openairdocs.org/sdr/C2XA00IA363.md): Bushing · grooved · Oct 4, 2000 · N15932 · Emb EMB145
  > IAH-DURING C-CHECK INSPECTION, THE RIGHT HAND HORIZONTAL STABILIZER AFT ATTACHMENT OUTBOARD BUSHING WAS FOUND TO BE PITTED AND CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUSHING IN ACCORDANCE WITH EMB145 M/M 20-10-08, AND THE AIRCRAFT WAS APPROVED
- [SDR C2XA00IA362](https://openairdocs.org/sdr/C2XA00IA362.md): Bushing · grooved · Oct 4, 2000 · N15932 · Emb EMB145
  > IAH-DURING C-CHECK INSPECTION, THE LEFT HAND HORIZONTAL STABILIZER AFT ATTACHMENT OUTBOARD BUSHING WAS FOUND TO BE HEAVILY GROOVED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUSHING IN ACCORDANCE WITH EMB145 M/M 20-10-08, AND THE AIRCRAFT WAS APPROVED FOR
- [SDR C2XA00IA361](https://openairdocs.org/sdr/C2XA00IA361.md): Bushing · grooved · Oct 4, 2000 · N15932 · Emb EMB145
  > IAH-DURING C-CHECK INSPECTION, THE LEFT HAND HORIZONTAL STABILIZER AFT ATTACHMENT INBOARD BUSHING WAS FOUND TO BE HEAVILY GROOVED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUSHING IN ACCORDANCE WITH EMB145 M/M 20-10-08, AND THE AIRCRAFT WAS APPROVED FOR R
- [SDR C2XA00IA360](https://openairdocs.org/sdr/C2XA00IA360.md): Bearing · corroded · Oct 4, 2000 · N15932 · Emb EMB145
  > IAH-DURING C-CHECK INSPECTION, THE VERTICAL STABILIZER TO HORIZONTAL STABILIZER LEFT HAND AND RIGHT HAND SPHERICAL BEARINGS WERE FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEARINGS IN ACCORDANACE WITH EMB145 M/M 55-37-00-400-801-A, AND
- [SDR AALA20001671](https://openairdocs.org/sdr/AALA20001671.md): Bearing · scored · Sep 27, 2000 · N7508 · Doug DC982
  > TUL - FOUND LEFT BEARING BORE SCORED, STATION XH 6.625, YH 70.95, ZH 7.25. HONED BORE TO 3.008 INCH AND INSTALLED NEW BUSHING PER CARD 3702 SRM 5502 FIG 12A. (M)
- [SDR C2XAOOIA378](https://openairdocs.org/sdr/C2XAOOIA378.md): Pin · corroded · Sep 26, 2000 · N15932 · Emb EMB145
  > REFERENCE OPEN SDR C2XAOOIA338-IAH-DURING C-CHECK INSPECTION, THE RIGHT HAND HORIZONTAL STABILIZER HINGE PIN WAS FOUND TO BE CORRODED. MX REMOVED/REPLACED THE AFFECTED PIN, AND A/C WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XAOOIA379](https://openairdocs.org/sdr/C2XAOOIA379.md): Pin · corroded · Sep 26, 2000 · N15932 · Emb EMB145
  > REFERENCE OPEN SDR C2XAOOIA337-IAH-DURING C-CHECK INSPECTION, THE LEFT HAND HORIZONTAL STABILIZER HINGE PIN WAS FOUND TO BE CORRODED. MX REMOVED/REPLACED AFFECTED PIN AND A/C WAS APPROVCED FOR RETURN TO SERVICE.
- [SDR C2XA00IA378](https://openairdocs.org/sdr/C2XA00IA378.md): Pin · corroded · Sep 26, 2000 · N15932 · Emb EMB145
  > REFERENCE OPEN SDR C2XAOOIA338 DURING C-CHECK INSPECTION RT HORIZONTAL STABILIZER HINGE PIN WAS FOUND TO BE CORRODED. MX REMOVED/REPLACED AFFECTED PIN, AND A/C WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA00IA338](https://openairdocs.org/sdr/C2XA00IA338.md): Pin · corroded · Sep 26, 2000 · N15932 · Emb EMB145
  > DURING C-CHECK INSPECTION R/H HORIZONTAL STABILIZER HINGE PIN WAS FOUND TO BE CORRODED. THIS SDR IS BEING FILED OPEN AWAITING FINAL CORRECTIVE ACTION.

Next page: https://openairdocs.org/jasc/5550/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 = '5550'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/jasc/5550/reports

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