# Service difficulty reports: JASC 5500

A list on [JASC 5500](https://openairdocs.org/jasc/5500.md).

Reports filed under 5500 · Empennage Structure, newest first.

Page 1 of 10 · 490 reports

- [SDR DXTA2026101910227](https://openairdocs.org/sdr/DXTA2026101910227.md): Erosion Shield · damaged · Oct 17, 2026 · N906QS · Cessna 680A
  > ON TAKEOFF ACCELERATING THROUGH 90KTS A LARGE BIRD FLEW AT THE AIRCRAFT AND VEERED TO THE LEFT SIDE OF THE NOSE AND UP AND OVER THE TOP OF THE FUSELAGE. ON POSTFLIGHT INSPECTED AND DISCOVERED DAMAGE TO THE VERTICAL STABILIZER. "CORRECTIVE ACTION" COMPLIED WITH
- [SDR IPXA2026090797965](https://openairdocs.org/sdr/IPXA2026090797965.md): Elevator · not reported · Sep 5, 2026 · N623UP · Boeing 7478F
  > ADD SDR FOR EO-85445-JIC2. ACCOMPLISHED EO-85445-JIC2.
- [SDR IPXA2026090797876](https://openairdocs.org/sdr/IPXA2026090797876.md): Elevator · not reported · Sep 5, 2026 · N623UP · Boeing 7478F
  > ADD SDR FOR EO-85445-JIC1. ACCOMPLISHED EO-85445-JIC1.
- [SDR DXTA2026060508322](https://openairdocs.org/sdr/DXTA2026060508322.md): Motor · faulted · Jun 2, 2026 · N540QS · Cessna 680A
  > WHEN CLIMBING, WITH THE AUTOPILOT ENGAGED, BETWEEN FL210 AND FL220, THE AMBER STAB TRIM MONITOR MESSAGE POSTED. WE RAN THE QRH AND MANUALLY USED THE PRIMARY STAB TRIM FOR AIRSPEED CHANGES. FODM WAS CONTACTED AND A DIVERSION WAS INITIATED. CORRECTIVE ACTION:
- [SDR J7SA2026041500479](https://openairdocs.org/sdr/J7SA2026041500479.md): Bracket · misinstalled · Apr 13, 2026 · N583FX · Bombdr BD1001A10
  > AIR TURN BACK DUE TO PITCH TRIM ACTUATION ON PILOT SIDE WORKED UNTIL REACHING 3.0 TRIM SETTING THEN STOPPED FUNCTIONING DURING TAKEOFF. PITCH TRIM WAS SET TO 5.3. CREW TRIED TO MOVE TWO TIMES WITH THE PILOT’S CONTROL TO NO AVAIL, THEN ACTIVATED CO-PILOT CONTRO
- [SDR U2RA2026051200017](https://openairdocs.org/sdr/U2RA2026051200017.md): Doubler · cracked · Mar 9, 2026 · N952CA · Boeing 747428
  > FINDING 002002 DOCUMENT FCD 744-53-0057-DURING C-CHECK 0.7" CRACK HAS EXTENDED FROM THE STOP HOLE OF THE PREVIOUS CRACK AT R/H STABILIZER UPPER LOBE DOUBLER. REPAIR WAS COMPLTED PER FAA 8100-9 DATED 0/21/2006 ON BOEING SERVICE REQUEST 202603060065-0011.
- [SDR AALA202603038969](https://openairdocs.org/sdr/AALA202603038969.md): Unknown · vibration · Feb 26, 2026 · N804AW · Airbus A319132
  > AIRCRAFT WAS GROUNDED: SIGNIFICANT AIRFRAME VIBRATION ABOVE 300KTS /.78M. FL250-280 IN CLIMB. ENGINE VIBRATION WAS NORMAL. WHEN F/CTL WAS CALLED UPTHE RUDDER TRAVEL LIMIT WAS AMBER VERY BRIEFLY. (OPEN)
- [SDR 8TNC202601220001](https://openairdocs.org/sdr/8TNC202601220001.md): Skin · cracked · Jan 22, 2026 · N405CP · Casa C212DF
  > DURING ROUTINE MAINTENANCE IN ANCHORAGE, AK (ANC), MAINTENANCE NOTED THAT (2EA.) FASTENERS COMMON TO THE HORIZONTAL STABILIZER LOWER SKIN & SPAR CHORD HAVE CRACKED OUT. THE CRACKS MEASURE.204” AND.242” LONG, RESPECTIVELY, AND THEY EMANATE IN THE OUTBOARD DIR
- [SDR IXXA20260104002](https://openairdocs.org/sdr/IXXA20260104002.md): Structure · damaged · Jan 4, 2026 · N457AZ · Boeing 767323
  > AREA 1 HAS CRACK INDICATION WHILE PERFORMING BS1809.5 HFEC OPEN HOLE SCANS PER ATI-EO-5300-767-07548, SB 767 53A0078 REV 6, FOUND DEFECTIVE HOLE AREA 1 THE LWR AFT HOLE WAS MISSING MATERIAL. REF 8100-9 202512125726-0004, TIN-TIN 25-0256-01C
- [SDR CALA2025090808603](https://openairdocs.org/sdr/CALA2025090808603.md): Skin · cracked · Aug 22, 2025 · N87527 · Boeing 737824
  > CRACK FOUND AT LEFT HORIZONTAL STAB LOWER SKIN AT HSS 147.90, INBD ROW. CRACK LENGTH: 1". ACCOMPLISHED PERMANENT REPAIR CATEGORY B AT LT HORIZONTAL STAB LOWER INSPAR SKIN AT HSS 147.90 IAW SRM 55-10-01-2R-11, REPAIR 11 FIGURE 204 DETAIL B.
- [SDR CALA2025050804557](https://openairdocs.org/sdr/CALA2025050804557.md): Rib · cracked · May 7, 2025 · N17752 · Boeing 737724
  > LH HORIZ STAB RIB #1 STIFFENER 3 CRACK. (REF AAR N/R 9962026) INSTALLED REPAIR PARTS AT L/H HORIZONTAL RIB 1 STIFFENER 3 WITH BMS 5-95 SEALANT AT 03/26/2024 AT 11:50 A.M, MIXED SEALANT AT 11:46 A.M CURE TIME IS 2:40 P.M, APPLIED FILLET SEAL AT REPAIR PARTS AT
- [SDR 2025FA0000203](https://openairdocs.org/sdr/2025FA0000203.md): Strake · corroded · Mar 24, 2025 · N587QS · Cessna 560XL
  > LH AND RH STRAKES HAVE SEVERAL AREAS OF CORROSION ON UPPER AND LOWER SURFACES. PERFORMED 4 EACH DOUBLER REPAIRS TO LH STRAKE AND PERFORMED 6 EACH DOUBLER REPAIRS TO RH STRAKE. ALL WORK WAS ACCOMPLISHED IN ACCORDANCE WITH EO NO: C56-53-0001 TITLED: MINOR REPAIR
- [SDR 2025FA0000201](https://openairdocs.org/sdr/2025FA0000201.md): Strake · corroded · Mar 22, 2025 · N587QS · Cessna 560XL
  > LH STRAKE TRAILING EDGE WEDGE FITTING
- [SDR VNAA20250320076](https://openairdocs.org/sdr/VNAA20250320076.md): Bonding Plate · debonded · Mar 19, 2025 · N509AE · Cndair CL6002C10
  > HN00199472 DISCREPANCY: PANEL 326CT HAS DISBONDED LIGHTNING DIVERTER PLATE WITH POSSIBLE CORROSION NEEDS FURTHER EVALUATION. CORRECTIVE ACTION: FABRICATED SERVICEABLE REPLACEMENT BONDING PLATE PN: 670-55-32-025-1 IAW STEPS 1-4 OF BOMBARDIER REO 670-55-32-025,
- [SDR DALA2025030201584](https://openairdocs.org/sdr/DALA2025030201584.md): Bushing · not reported · Feb 25, 2025 · N3737C · Boeing 737832
  > (LOG 0829464) ALL 8 BUSHINGS ON AFT PRIMARY AND FAIL SAFE FITTING MUST BE REPLACED. R/R ALL 8 BUSHINGS ON AFT PRIMARY AND FAILSAFE FITTINGS PER PRI 624280-14, C/W ALL RII ITEMS, REF ERA 624280 REV 0, PRI REV 5.
- [SDR QXEA2024120400289](https://openairdocs.org/sdr/QXEA2024120400289.md): Fitting · broken · Nov 29, 2024 · N634QX · Emb ERJ170200LR
  > FLT CTRL NO DISPATCH ON EICAS DURING CAPT FLIGHT CONTROL CHECK AFTER ENGINE START.FOUND FAULTS 27030378FCS & 22110198PB2. REMOVED FROM SERVICE. R+R P-ACE #1 REF. E175 AMM 27-03-03-000/400-801-A. NO HELP. WHEN TROUBLESHOOTING A FCND, FOUND LH ELEVATOR OB LVDT B
- [SDR DALA2024110110572](https://openairdocs.org/sdr/DALA2024110110572.md): Access Panel · chafed · Oct 31, 2024 · N178DZ · Boeing 767332
  > SHIP 1708 RH STABILIZER BODY LOWER SEAL ACCESS PANEL FWD CUTOUT WEAR STRAP FOUND CHAFED. CORRECTIVE ACTION: THE WEAR STRAP REPAIRED AS PER B767-300 SRM53-80-01 (0637535)
- [SDR N6WA2024101301](https://openairdocs.org/sdr/N6WA2024101301.md): Fairing · damaged · Oct 13, 2024 · N556GJ · Cndair CL6002C11
  > TAIL FAIRING DAMAGED. REPLACED AFT FAIRING IAW CRJ AMM 55-32-86.
- [SDR SWIA20250113004](https://openairdocs.org/sdr/SWIA20250113004.md): Isolation Valve · chafed · Oct 4, 2024 · N932EV · Cndair CL6002B19
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA74078-601R-53-61-7737 932EV MXCODEID59444-PR - FOUND SMALL CHAFE DAMAGE ON WINTERIZATION BEHIND THE 10TH STAGE ISOLATION VALVE ON THE FS 621 BULKHEAD VERTICAL STIFFENER AT BL 0.00. COMPLIED WITH REO 601R-53-61-7737 REV
- [SDR SWAA2024093042690](https://openairdocs.org/sdr/SWAA2024093042690.md): Strut · cracked · Sep 26, 2024 · N476WN · Boeing 7377H4
  > FOUND CRACK ON TRF PN 340-166-210-0 SN PA179695 STRUT 16 AREA C2 THAT MEASURES.375' IN LENGTH.<[01] C/W EA M-21-172-00810 TRIGGERING TRF MOUNT INSPECTION 7256-I-14340 FOR LARGEST CUMULATED CRACK FINDINGS FROM 0.28 INCH TO LESS THAN 0.39 INCH IN LENGTH
- [SDR 2024FA0000736](https://openairdocs.org/sdr/2024FA0000736.md): Bolt · corroded · Sep 22, 2024 · Boeing 78710
  > 9V-SCF IS CURRENTLY IN HANGAR. DURING THE ACCOMPLISHMENT OF THE ADSI IB78J550001 INSPECTION OF THE TENSION BOLT HOLES, 2 GOUGES WERE FOUND ON HOLE #16, AFTER CORROSION REMOVAL.
- [SDR 2024FA0000731](https://openairdocs.org/sdr/2024FA0000731.md): Bolt · corroded · Sep 22, 2024 · Boeing 78710
  > 9V-SCF IS CURRENTLY IN HANGAR. DURING THE ACCOMPLISHMENT OF THE ADSI IB78J550001 INSPECTION OF THE TENSION BOLT HOLES, CORROSION WAS FOUND ON HOLE #14 AND #16.
- [SDR JR2R20240829301](https://openairdocs.org/sdr/JR2R20240829301.md): Fitting · damaged · Aug 29, 2024 · N87318 · Emb ERJ170200LR
  > LH FR100 FITTING SAFE PIN HOLE HAS EVIDENCE OF ELONGATING. REPAIRED
- [SDR DALA2024080507777](https://openairdocs.org/sdr/DALA2024080507777.md): Unknown · damaged · Aug 1, 2024 · N948DZ · Boeing 7379GPER
  > (LOG 6207922) WHILE WORKING INBD STAB TRIM WRITE UP FOUND DAMAGE. C/W ERA 619788-14 REV. ORIG.
- [SDR 2024FA0000561](https://openairdocs.org/sdr/2024FA0000561.md): Attach Fitting · corroded · Jul 28, 2024 · Boeing 78710
  > WHILE ACCOMPLISHING FAA AD 2022-15-01, FOUND HOLE #1 AND #4 TO HAVE CORROSION
- [SDR JGVR202404050002](https://openairdocs.org/sdr/JGVR202404050002.md): Strake · corroded · Apr 5, 2024 · N678QS · Cessna 560XL
  > DURING THE VENTRAL STRAKE COIN TAP TEST FOUND MULTIPLE SPOT OF SURFACE LEVEL CORROSION. PERFORM REPAIR TO RH STRAKE CORROSION. COMPLIED WITH RFTS-110419 REV.0 DATED MAR 29, 2024 TO REPAIR THE LEVEL 2 CORROSION ON THE FWD IB LEADING EDGE AND UPPER DRAG ANGLE OF
- [SDR JGVR202404050001](https://openairdocs.org/sdr/JGVR202404050001.md): Strake · corroded · Apr 5, 2024 · N678QS · Cessna 560XL
  > DURING THE VENTRAL STRAKE COIN TAP TEST FOUND MULTIPLE SPOT OF SURFACE LEVEL CORROSION. PERFORM REPAIR TO LH STRAKE CORROSION. COMPLIED WITH RFTS-110424 REV.0 DATED MAR 29, 2024 TO REPAIR THE LEVEL 2 CORROSION ON THE FWD IB LEADING EDGE OF THE LH STRAKE BY FAB
- [SDR AALA202403183669](https://openairdocs.org/sdr/AALA202403183669.md): Skin · cracked · Mar 13, 2024 · N902AN · Boeing 737823
  > AIRCRAFT IN BASE MAINTENANCE: FOUND CRACK IN AFT LEFT HAND OF SECTION 48 JUST AFT OF BS 1138 MEASURING 2 INCHES LENGTH BY 0.063 IN WIDTH AND 0.30 IN DEPTH. ITEM MINOR IN NATURE. PERFORMED A GENERAL VISUAL INSPECTION OF AREA, FOUND DAMAGE WITHIN LIMITS. PREFO
- [SDR DALA2024030503014](https://openairdocs.org/sdr/DALA2024030503014.md): Bolt · loose · Mar 4, 2024 · N418DX · Airbus A330941
  > SHIP 3418 THS R/H LOWER ATTACHMENT TO THE CARDAN HAS A LOOSE BOLT. CORRECTIVE ACTION: RETORQUED BOLT AND REPLACED TAB WASHER REF A330 AMM 27-44-51. OK FOR SERVICE. (0230104)
- [SDR DALA2024011600636](https://openairdocs.org/sdr/DALA2024011600636.md): Unknown · unknown · Jan 15, 2024 · N352DN · Airbus A321211
  > SHIP 3052 WEAR ON O/B SERVO CONTROL BUSHING ON ELEVATOR LT ATTACH FITTING I/B LUG (1 E/A). CORRECTIVE ACTION: REPLACED BUSHING (1 EA) ON OUTBOARD ACTUATOR I/B LUG OF LH ELEVATOR PER A321 CMM 55-21-15. (0155062)
- [SDR DALA2024011600635](https://openairdocs.org/sdr/DALA2024011600635.md): Unknown · unknown · Jan 15, 2024 · N352DN · Airbus A321211
  > SHIP 3052 WEAR ON I/B SERVO CONTROL BUSHING ON ELEVATOR L/H ATTACH FITTING O/B LUG. CORRECTIVE ACTION: REPLACED BUSHING (1 EA) ON INBOARD ACTUATOR O/B LUG OF LH ELEVATOR AS PER A321 CMM 55-21-15. OK FOR SVC. (0155057)
- [SDR DALA2024011600634](https://openairdocs.org/sdr/DALA2024011600634.md): Unknown · unknown · Jan 15, 2024 · N352DN · Airbus A321211
  > SHIP 3052 WEAR ON I/B SERVO CONTROL BUSHING ON ELEVATOR LT ATTACH FITTING I/B LUG (1 E/A). CORRECTIVE ACTION: REPLACED BUSHING (1 EA) ON INBOARD ACTUATOR I/B LUG OF LH ELEVATOR PER A321 CMM 55-21-15. (0155054)
- [SDR DALA2024011600633](https://openairdocs.org/sdr/DALA2024011600633.md): Unknown · unknown · Jan 15, 2024 · N352DN · Airbus A321211
  > SHIP 3052 WEAR ON O/B SERVO CONTROL BUSHING ON ELEVATOR L/H ATTACH FITTING O/B LUG. CORRECTIVE ACTION: REPLACED BUSHING (1 EA) ON OUTBOARD ACTUATOR O/B LUG OF LH ELEVATOR AS PER A321 CMM 55-21-15. (0155049)
- [SDR DALA2024011600632](https://openairdocs.org/sdr/DALA2024011600632.md): Unknown · unknown · Jan 15, 2024 · N352DN · Airbus A321211
  > SHIP 3052 WEAR ON INBOARD ACTUATOR FITTING IB LUG PLAIN BUSHING ON RH ELEVATOR (1 EA). CORRECTIVE ACTION: REPLACED BUSHING (1 EA) ON INBOARD ACTUATOR I/B LUG OF RH ELEVATOR AS PER AIRBUS CMM 55-21-15. (0155045)
- [SDR 2023FA0000856](https://openairdocs.org/sdr/2023FA0000856.md): Unknown · unknown · Dec 30, 2023 · N162GB · Gulstm 200
  > DURING G200 ECS ZONAL INSPECTION SEVERAL FASTENERS FOUND DISCOLORED WITH POSSIBLE EVIDENCE OF ARCING IN ECS COMPARTMENT AT STN;14783MM,FRAME 51 (FWD. BEAM PYLON CAP) PN 4AS3177202-001
- [SDR 2023FA0000744](https://openairdocs.org/sdr/2023FA0000744.md): Fitting · corroded · Nov 6, 2023 · N5017N · Boeing B17G
  > UPON REMOVAL OF HORIZONTAL STABILIZERS AND VERTICAL FIN ON THE AIRCRAFT IT WAS NOTED THAT THEIR ARE SEVERAL CAST FITTINGS LOCATED INSIDE THE EMPENNAGE THAT WERE SHOWING SINGES OF SURFACE CORROSION AS WELL AS POSSIBLE INNER GRANULAR CORROSION ON A COUPLE OF THE
- [SDR SWAA2023112013478](https://openairdocs.org/sdr/SWAA2023112013478.md): Door Latch · corroded · Oct 22, 2023 · N8673F · Boeing 7378H4
  > STABILIZER TRIM ACCESS DOOR LATCH MECHANISM HARDWARE/COMPONENTS HAS CORROSION.<[01] REMOVED AND REPLACED STABILIZER TRIM ACCESS DOOR 311BL LATCH MECHANISM REF SRM 51-40-02; AND AMM 52-41-11.;[02] CORRECTION: REMOVED AND REPLACED STABILIZER TRIM ACCESS DOOR 311
- [SDR DALA2023092907996](https://openairdocs.org/sdr/DALA2023092907996.md): Fitting · damaged · Sep 23, 2023 · N172DZ · Boeing 767332
  > ERA 611846-14AD ISSUED FOR REPAIR TO LH AND RH H STAB PIVOT FITT ING ATTACH HOLE REWORK. DTA DTE DAMAGE TOLERANCE ANALYSIS IS REQ UIRED. CORRECTIVE ACTION: CPER ER/A 611846-14AD REV A, DTE STAGE 2 AND 3 ACCOMPLISHED.
- [SDR ASAA2023090645088](https://openairdocs.org/sdr/ASAA2023090645088.md): Rib · cracked · Sep 6, 2023 · N611AS · Boeing 737790
  > UPON INSTALL OF SKIN REPAIR STAB RIB WAS FOUND CRACKED AT AFT MOST HOLE IN RADIUS AT R/H STAB STA 92. GROUNDED - YES. REMOVED AND REPLACED RIB AT STA 92 IAW B737-700 SRM 51-40-02-0G-0.
- [SDR UIEA2023082900801](https://openairdocs.org/sdr/UIEA2023082900801.md): Unknown · unknown · Aug 28, 2023 · N446MC · Boeing 7474B5F
  > MDDR 188056, PERMANENT REPAIR OF LH ELEVATOR ON OR BEFORE 25 F/C PER EO 4455A183(<P>1) REMOVE THE DAMAGE MATERIAL, CLEAN & MEASURE THE DAMAGE AREA (L: 8.5", W: 6", D: 3 PLIES, 36" FROM OUTBD EDGE AT T/E) BOND THE 3 REPAIR PLIES (L: 11.5", W: 2.2") WITH FILM AD
- [SDR IPXA2023082794035](https://openairdocs.org/sdr/IPXA2023082794035.md): Support · cracked · Aug 19, 2023 · N135UP · Airbus A300F4622R
  > INSPECTION TYPE:1CSUPPORT BRACKET P/N A5517155320300 IS CRACKED.REMOVED AND REPLACED IAW SRM 51-40-21.
- [SDR P5CA2023080200058](https://openairdocs.org/sdr/P5CA2023080200058.md): Unknown · unknown · Aug 18, 2023 · N857GT · Boeing 74787UF
  > LH HORI. STAB. TIP SUPPORT U CHNNEL FOUND CRACK(<P>BONDED NEW U CHANNEL PER RI NO: RI-55-10-16388 REV.A</P>)
- [SDR P5CA2023081300073](https://openairdocs.org/sdr/P5CA2023081300073.md): Unknown · unknown · Aug 18, 2023 · N857GT · Boeing 74787UF
  > RH HORIZ STAB AFT SUPPORT CHANNEL FOUND CRACK(<P>RH HORIZ STAB ACCESS PANEL 344GB AFT SUPPORT CHANNEL REPLACED AND INSTALLED AS PER RI-55-10-16398 REV A DATE 15 AUG 2023.</P>)
- [SDR AALA202308112457](https://openairdocs.org/sdr/AALA202308112457.md): Stabilizer · warning light · Aug 10, 2023 · N976NN · Boeing 737823
  > AIRCRAFT WAS NOT GROUNDED: AN EMERGENCY WAS DECLARED INTO MIA DUE TO STABILIZER TRIM FAILURE WITH BOTH AUTPILOTS ON AND OFF. FLIGHT CREW ALSO REPORTED PERIODIC SPEED TRIM FAILURE LIGHT ILLUMINATED. THE AIRCRAFT LANDED SAFELY AT MIA WITHOUT FURTHER INCIDENT. MA
- [SDR ENHA20230801002](https://openairdocs.org/sdr/ENHA20230801002.md): Unknown · unknown · Aug 1, 2023 · N9310F · Cessna 208B
  > DURING SCHEDULED INSPECTIONS PER CESSNA TASK 53-10-00-257,A CRACK WAS NOTED AT THE HORIZONYAT RH AFT FITTING.
- [SDR SWAA2023072882387](https://openairdocs.org/sdr/SWAA2023072882387.md): Seal · cracked · Jul 26, 2023 · N8657B · Boeing 7378H4
  > RIGHT HORIZONTAL STAB FWD UPPER SLIDING SEAL CRACKED.<[01] REMOVED AND REPLACED RIGHT HORIZONTAL STAB FWD UPPER SLIDING SEAL PER AMM 53-31-31.
- [SDR SWAA2023072881938](https://openairdocs.org/sdr/SWAA2023072881938.md): Seal · cracked · Jul 25, 2023 · N233LV · Boeing 7377H4
  > THE RIGHT UPPER HORIZONTAL STAB TO BODY FRONT SLIDING SEAL IS CRACKED.<[01] REMOVED AND REPLACED SEAL PER AMM 53-31-31
- [SDR SWIA202309080723](https://openairdocs.org/sdr/SWIA202309080723.md): Unknown · corroded · Jul 23, 2023 · N978SW · Cndair CL6002B19
  > AFTER REMOVAL OF R/H ELEVATOR FITTING AT BL15.25, FITTING WAS DIS-ASSEMBLED TO EVALUTE PRIOR TO NEW BEARING INSTALLATION AND FOUND CORROSION AND PITTING INSIDE BOTH SIDES OF BEARING BORE. (C-CHECK RO 9/6/2023) R/H ELEVATOR FITTING LOCATED AT BL 15.25 HA
- [SDR SWI202309008321](https://openairdocs.org/sdr/SWI202309008321.md): Unknown · corroded · Jul 22, 2023 · N978SW · Cndair CL6002B19
  > UPON REMOVAL ON JOB HN103215 CAMP #26917265, FOUND L/H ELEVATOR L/E HINGE FITTING ASSY P/N 600-24043-1 AT ES16.52 TO HAVE PITTING CORROSION IN BEARING BORES OF BOTH FITTING HINGE HALVES. REPLACE HINGE FITTING ASSY P/N 600-24043-1. (C-CHECK RO 9/6/2023)
- [SDR SWIA202309080718](https://openairdocs.org/sdr/SWIA202309080718.md): Unknown · gouged · Jul 18, 2023 · N978SW · Cndair CL6002B19
  > RH ELEVATOR INBD HINGE GOUGED (C-CHECK RO 9/6/2023) REMOVED GOUGE FROM RH ELEVATOR INBD HINGE, WITHIN LIMITS. RECEIVED AND COMPLIED WITH MHIRJ REO 601R-55-11-748 REV --A, DATED 2023-08-18. SEE CONTINUATION FOR FURTHER DETAILS. COMPLIED WITH 51-900-1003

Next page: https://openairdocs.org/jasc/5500/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 = '5500'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/jasc/5500/reports

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