# Service difficulty reports: Cessna 188A

A list on [Cessna 188A](https://openairdocs.org/model/cessna-188a.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 98 reports

- [SDR CA150625003](https://openairdocs.org/sdr/CA150625003.md): Actuator · malfunctioned · Jun 24, 2015 · Lkheed 188A · Propeller Controlling System
  > (CAN) THE NR 2 ENG LOST POWER ON THE OVERSHOT FROM A BOMB RUN & WAS SHUTDOWN, RETURNED TO BASE. FOUND THE NR 2 PROPELLER ROTARY ACTUATOR TO BE OVER TRAVELLING. REPLACED U S ACTUATOR WITH A SERVICEABLE UNIT & RETURNED THE ACFT TO SERVICE.
- [SDR CA140707015](https://openairdocs.org/sdr/CA140707015.md): Valve · malfunctioned · Jul 3, 2014 · Lkheed 188A · Compressor Bleed Control
  > (CAN) ON TAKEOFF LOW HORSEPOWER, HIGH FUEL FLOW, AND HIGH T.I.T. WERE OBSERVED. TAKEOFF WAS ABORTED PRIOR TO BRAKE RELEASE. MAINTENANCE FOUND SPEED SENSE VALVE NOT CLOSING 5TH AND 10TH STAGES. VALVE REPLACED.
- [SDR CA140702010](https://openairdocs.org/sdr/CA140702010.md): Gasket · leaking · Jun 24, 2014 · Lkheed 188A · Hydraulic System, Main
  > (CAN) NR 2 HYD SYS LOST ALL FLUID QTY. ACFT RETURNED TO THE AIRPORT. INSPECTED NR 2 HYDRAULIC SYSTEM, LEAK FOUND AT FILTER HOUSING, LEAKING GASKET FOUND AND REPLACED.
- [SDR CA130813004](https://openairdocs.org/sdr/CA130813004.md): Controller · malfunctioned · Aug 11, 2013 · Lkheed 188A · Propeller Controlling System
  > (CAN) NR 4 ENGINE RPM DECAYED TO BOTTOM OF NORMAL RANGE AT HIGH POWER DURING TAKEOFF, BOMBING BUT WAS NORMAL IN CLIMB AND CRUISE. AFTER TROUBLESHOOTING THE ROTARY ACTUATOR WAS REPLACED AND PROBLEM WAS FIXED.
- [SDR CA130729021](https://openairdocs.org/sdr/CA130729021.md): Regulator · malfunctioned · Jul 26, 2013 · Lkheed 188A · Propeller Controlling System
  > (CAN) PROPELLER FAILED TO GOVERN RPM IN FLIGHT. UPON ADVANCEMENT OF POWER FOR ASSOCIATED ENGINE FCU HAD TO LIMIT ENGINE RPM VIA FUEL TOPPING GOVERNOR. MAINTENANCE CREW REPLACED GOVERNOR VALVE OF PROPELLER AND COMPLETED A PITCH LOCK CHECK AND DETERMINED PROPE
- [SDR CA130515013](https://openairdocs.org/sdr/CA130515013.md): Fire Detector · malfunctioned · May 14, 2013 · Lkheed 188A · Fire Detection
  > (CAN) PILOTS REPORTED A ZONE 1 FIRE INDICATION APPROXIMATELY 20 MILES FROM THE AIRPORT WHILE INBOUND FOR LANDING. AFTER PULLING THE POWER BACK TO IDLE NO CHANGE. THEY E-HANDLED THE ENGINE AND THE INDICATION WENT OUT IMMEDIATELY. ON THE GROUND WE INSPECTED VI
- [SDR CA130513023](https://openairdocs.org/sdr/CA130513023.md): Transfer Tube · misinstalled · May 9, 2013 · Lkheed 188A · Propeller Assembly
  > (CAN) PROPELLER NOT REGULATING OIL PRESSURE IN FLIGHT. RPM WOULD SWING WITH POWER LEVER CHANGES. UPON INVESTIGATION IT WAS DISCOVERED THAT AN O-RING AND BACK-UP RING COMBINATION INSTALLED ON AN INTERNAL TRANSFER TUBE ASSY IN THE PROPELLER HUB WERE REVERSED CA
- [SDR CA110602005](https://openairdocs.org/sdr/CA110602005.md): Pulley · broken · Jun 1, 2011 · Lkheed 188A · Trailing Edge Flap Control System
  > DURING INITIAL TAXI FOR A MX TEST FLIGHT, THE FLIGHT CREW RECEIVED A FLAP ASYMMETRIC WARNING. THE ACFT WAS RETURNED TO THE HANGAR WHERE UPON INITIAL INVESTIGATION IT WAS FOUND THAT THE RT FLAP ASYMMETRIC CABLE LOCATED IN THE RT FLAP BAY WAS BROKEN WITH SIGNS O
- [SDR CA100531005](https://openairdocs.org/sdr/CA100531005.md): Nut · broken · May 18, 2010 · Lkheed 188A · Turbine Section
  > AFTER TAKEOFF FOR A FIRE DISPATCH, THE NR 1 FIRE LIGHT AND BELL SOUNDED. THE LIGHT AND BELL QUIT AFTER THE POWER WAS REDUCED FROM TAKEOFF POWER. AFTER LANDING, MX FOUND THAT THE POWER TURBINE ON THE NR 1 ENGINE HAD FAILED. THE NEXT DAY THE ACFT WAS FLOWN O
- [SDR CA090727010](https://openairdocs.org/sdr/CA090727010.md): Engine · power loss · Jul 26, 2009 · Lkheed 188A · Engine (Turbine/Turboprop)
  > DISPATCHED FOR FIRE ACTION. AFTER RETARDANT DROP NR 2 RPM DROOPED TO 13,500. RPM BEGAN TO HUNT BETWEEN 13500, 13300 (13820 NORMAL). NR 2 ENGINE SHUTDOWN AND SECURED IAW COMPANY SOP. ONE ENG INOP LANDING CARRIED OUT. MX IS TROUBLESHOOTING.
- [SDR CA090615011](https://openairdocs.org/sdr/CA090615011.md): Module · burned out · Jun 13, 2009 · Lkheed 188A · Propeller Synchronizer Section
  > (CAN) SEVEN MINUTES FROM AIRPORT, CREW NOTICED SMOKE COMING FROM ELECTRICAL BAY. WITH NO SYSTEMS FAILED, THE CREW RETURNED TO DEPARTURE WITH NO INCIDENTS. MX FOUND NR 1 PROP PHASE SYNC MODULE HAD BURNED OUT. ALL ACFT WIRES WERE CHECKED OUT TO BE OK, THE SYS
- [SDR CA080422003](https://openairdocs.org/sdr/CA080422003.md): Coupler · unknown · Apr 20, 2008 · Lkheed 188A · Accessory Gearboxes
  > (CAN) DURING START SEQUENCE OF NR 4 ENGINE, IT WAS OBSERVED THAT RPM AND ACCELERATION CLIMBED TOO FAST, BEFORE LIGHT OFF, ENGINE START ABORTED AND FOUND ENGINE DECOUPLED FROM GEARBOX. SUSPECT TORQUE SHAFT COUPLER (TC NR 20080422003)
- [SDR CA070918002](https://openairdocs.org/sdr/CA070918002.md): Panel · cracked · Sep 16, 2007 · Lkheed 188A · Wing, Plate/Skin
  > (CAN) AFTER A (WATER - FIRE SUPPRESSION) BOMBING MISSION, FUEL WAS FOUND LEAKING FROM A CRACK THAT WAS COMING FROM AN OLD REPAIR. THE A/C WAS DOWN LOADED WITH WEIGHT AND THE A/C WAS FERRIED TO THE COMPANY MAINTENANCE STATION. (TC NR 20070918002)
- [SDR CA060613003](https://openairdocs.org/sdr/CA060613003.md): Seal · leaking · Jun 11, 2006 · Lkheed 188A · Turbine Engine Oil System
  > (CAN) AFTER A WATER BOMBING RUN CLIMB OUT NR 2 ENGINE WAS SHOWING TWO GALLONS LOW ON OIL. THERE WAS NO OTHER ABNORMAL INDICATIONS, THE CREW DID A PRECAUTIONARY SHUT DOWN. MAINTENANCE FOUND THE SCAVENGE PUMP SEAL TO BE LEAKING OIL BY, THE SEAL WAS REPLACED AND
- [SDR CA050908003](https://openairdocs.org/sdr/CA050908003.md): Coupling · broken · Sep 5, 2005 · Lkheed 188A · Trailing Edge Flap Control System
  > (CAN) THE A/C HAD FINISHED IT'S THIRD DROP ON A FIRE BOMBING PRACTICE, FLAPS WOULD NOT RETRACT AND THE FLAP ASYMMETRIC LIGHT WAS ON. THE FLAP ASYMMETRY CHECKLIST WAS COMPLETED AND THE A/C RETURNED TO BASE. MAINTENANCE FOUND A BROKEN TORQUE TUBE COUPLING, THE
- [SDR ZIAA04082](https://openairdocs.org/sdr/ZIAA04082.md): Fire Loop · false indication · Sep 28, 2004 · N346HA · Lkheed 188A · Fire Detection
  > SHUTDOWN NR 3 ENGINE DUE TO ZONE 1 FIRE WARNING AT 2004Z. DISCHARGED FIRE BOTTLES. REMOVED AND REPLACED ZONE 1 FIRE LOOP IAW L188 MM 26-1-0. NO FIRE WARNING NOTED ON EXTENDED GROUND RUN AT 847 DEGREES.
- [SDR ZIAA04067](https://openairdocs.org/sdr/ZIAA04067.md): Control Handle · out of rig · Aug 4, 2004 · N343HA · Lkheed 188A · Landing Gear Selector
  > LANDING GEAR HANDLE APPEARS NOT TO GO TO THE FULL UP POSITION. RIGHT MAIN GEAR UNSAFE LIGHT STAYS ON. RIGGED RIGHT LANDING GEAR UPLOCK MECHANISM IAW L-188 MM 32-1-0. ZIAA (M)
- [SDR CA040720005](https://openairdocs.org/sdr/CA040720005.md): Propeller · malfunctioned · Jul 17, 2004 · Lkheed 188A · Propeller Governor
  > PROPELLER OVERSPEED ON DESCENT INTO XXXX, THE ENGINE WAS SHUT DOWN AND AIRCRAFT LANDED WITHOUT INCIDENT. PROP ASSEMBLY WAS CHANGED, GROUND RUN AND PITCH LOCK TESTED SERVICABLE. AIRCRAFT WAS RETURNED TO SERVICE.
- [SDR ZIAA03005](https://openairdocs.org/sdr/ZIAA03005.md): Panel · corroded · Nov 3, 2003 · N346HA · Lkheed 188A · Wing, Plate/Skin
  > YIP - PLANK NR 3 JUST AFT OF 2-3 PLANK SEAM CORROSION BETWEEN RISERS AT BL61R, CENTER DRY BAY, LOWER SURFACE. REMOVED CORROSION AND TREATED AREA. REPAIRED PER LOCKHEED S/B 678 DWG 841795. (M)
- [SDR ZIAA03004](https://openairdocs.org/sdr/ZIAA03004.md): Panel · cracked · Nov 3, 2003 · N346HA · Lkheed 188A · Wing, Plate/Skin
  > CRACK NOTED IN CENTER DRY BAY RIGHT WING AT PLANK SEAM 5-6 AT BL37R. ROUTED OUT CRACK AND INSTALLED FILLET PER L-188 SRM 51-2-7. REPAIRED PER L-188 SRM 57-2-1 FIG 3 SHEET 15. (M)
- [SDR ZIAA03003](https://openairdocs.org/sdr/ZIAA03003.md): Relay · overheated · May 21, 2003 · N5512 · Lkheed 188A · AC Power Distribution System
  > LANDED IN TORONTO DUE TO ELECTRICAL SMOKE COMING FROM BEHIND COCKPIT CIRCUIT BREAKER PANEL. REMOVED AND REPLACED NR 2 MAIN DC BUS REVERSE CURRENT CUTOUT RELAY IAW L-188 MM CPT 24-0. ALL SYSTEM CHECK NORMAL. (M)
- [SDR ZIAA03002](https://openairdocs.org/sdr/ZIAA03002.md): Skin · corroded · Feb 18, 2003 · N343HA · Lkheed 188A · Wing, Plate/Skin
  > YIP - FOUND CORROSION ON LEFT WING LOWER SURFACE NR 4 WING PLANK TRAILING EDGE BETWEEN APPROXIMATE LWS 448 AND LWS 533. REMOVED CORRODED SECTION OF NR 4 WING PLANK TRAILING EDGE PER ZANTOP DWG S59-R01. (M)
- [SDR CA020829006](https://openairdocs.org/sdr/CA020829006.md): Structure · cracked · Aug 8, 2002 · Lkheed 188A · Wing Main, Frame Structure
  > (CAN) CRACK ALONG EXISTING PATH FOUND. AIRCRAFT RETURNED TO MAINTENANCE BASE. CRACK IS OUTBOARD OF BL-165 19 INCHES
- [SDR ZIA2002F00000](https://openairdocs.org/sdr/ZIA2002F00000.md): Battery · discharged · May 14, 2002 · N346HA · Lkheed 188A · Battery/Charger System
  > IN CRUISE, EN-ROUTE, LOST (A) BUS IN FLIGHT. LOST ALL RADIOS BOTH COMMS AND BOTH NAVS. OVERWEIGHT LANDING. RESET ALL MAIN FEEDER C/BS OPS. CHECKED GOOD ON GROUND RUN-UP. REMOVED MAIN AC BATTERY AND REPAIRED BATTERY CONNECTOR, OPS CHECKED GOOD COMPLIED WITH
- [SDR TM92002F00000](https://openairdocs.org/sdr/TM92002F00000.md): Battery · discharged · May 14, 2002 · N436HA · Lkheed 188A · Battery/Charger System
  > (LEAD ACID BATTERY) IN CRUISE, ENROUTE LOST (A) BUS IN FLIGHT. LOST ALL RADIOS, BOTH COMMS AND BOTH NAVS. OVERWEIGHT LANDING. RESET ALL MAIN FEEDER C/BS. OPS CHECKED GOOD ON GROUND RUN-UP. REMOVED AND REPLACED MAIN AIRCRAFT BATTERY CONNECTOR, OPS CHECKED
- [SDR ZIAA06001](https://openairdocs.org/sdr/ZIAA06001.md): Plank · cracked · Jun 24, 2001 · N346HA · Lkheed 188A · Wing, Plate/Skin
  > NR 2 PLANK CRACKED. LEFT WING INBOARD OF CENTER RISER. (M)
- [SDR ZIAA00017](https://openairdocs.org/sdr/ZIAA00017.md): Panel · cracked · Nov 4, 2000 · N346HA · Lkheed 188A · Wing, Plate/Skin
  > YIP - LEFT DRY BAY UPPER SURFACE, CRACK INDICATION COMING FROM FASTENER HOLE BETWEEN RISERS 46-47 AT WS 200, APPROX 1.5 INCH IN LENGTH. CLEANED CRACK PER L-188 SRM 51-2-7 PAGE 2. REPAIRED PER ZANTOP DWG M16-R01. (M)
- [SDR ZIAA00011](https://openairdocs.org/sdr/ZIAA00011.md): Pump · leaking · Sep 30, 2000 · N346HA · Lkheed 188A · Hydraulic Pump (Electric/Engine), Main
  > YIP - IN FLIGHT NR 1A PUMP LOW PRESSURE LIGHT CAME ON, TURNED OFF. REMOVED AND REPLACED NR 1A HYD PUMP PER CARD N29-01. OPS AND LEAK CHECKS GOOD ON GROUND. (M)
- [SDR ZIAA00012](https://openairdocs.org/sdr/ZIAA00012.md): Stringer · corroded · Sep 28, 2000 · N344HA · Lkheed 188A · Fuselage Main, Longeron/Stringer
  > YIP - LONGERON NR 29 ON RIGHT FUSELAGE STATION 416 FOUND CORRODED. REPAIRED LONGERON PER L-188 DRAWING NR L55-R01. (M)
- [SDR 20010112SG015](https://openairdocs.org/sdr/20010112SG015.md): Fitting · worn · Sep 28, 2000 · N344HA · Lkheed 188A · Cargo/Baggage Doors
  > YIP - FORWARD CARGO DOOR, DOOR MOUNTED LINK ARM HAS EXCESS MOTION AT DOOR ATTACH POINT. REPAIRED FORWARD CARGO DOOR ATTACH POINTS IAW ZANTOP DRAWING NR L84-R01. REF ZIAA00013. (M)
- [SDR ZIAA00013](https://openairdocs.org/sdr/ZIAA00013.md): Fitting · worn · Sep 28, 2000 · N344HA · Lkheed 188A · Cargo/Baggage Doors
  > YIP - FORWARD CARGO DOOR, DOOR MOUNTED LINK ARM HAS EXCESS MOTION AT DOOR ATTACH POINT. REPAIRED FORWARD CARGO DOOR ATTACH POINTS IAW ZANTOP DRAWING NR L84-R01. (M)
- [SDR ZIAA00015](https://openairdocs.org/sdr/ZIAA00015.md): Skin · corroded · Sep 14, 2000 · N344HA · Lkheed 188A · Fuselage Main, Plate/Skin
  > YIP - EVIDENCE OF CORROSION ON SEVERAL AREAS OF SKIN BETWEEN FS 445-588 RIGHT SIDE. NUMEROUS AREAS OF SURFACE CORROSION ON STRINGERS UNDER SKIN. REMOVED SKIN SECTION, FOUND CORROSION TO BE BEYOND LIMITS. FABRIATED NEW SKIN PANEL. REPLACED SKIN PER L-188 SR
- [SDR ZIAA00014](https://openairdocs.org/sdr/ZIAA00014.md): Stringer · cracked · Sep 13, 2000 · N344HA · Lkheed 188A · Fuselage Main, Longeron/Stringer
  > YIP - FOUND FUSELAGE STATION 549 BELOW STRINGER 51 CRACKED ON RIGHT SIDE. REPAIRED CRACKED STRINGER IAW L-188 53-2-3 SRM. (M)
- [SDR ZIAA00010](https://openairdocs.org/sdr/ZIAA00010.md): Panel · cracked · Jul 27, 2000 · N5512 · Lkheed 188A · Wing, Plate/Skin
  > YIP - LEFT DRY BAY, UPPER SURFACE, CRACK INDICATION BETWEEN NR 45-46 RISERS AT LT WS 200, CRACK SIZE 1.25 BY.375. CLEANED OUT CRACK PER L-188 SRM 51-2-7 PAGE 2. REPAIRED PER L-188 SRM 57-2-1 PAGE 19. (M)
- [SDR ZIAA00009](https://openairdocs.org/sdr/ZIAA00009.md): Panel · cracked · Jul 27, 2000 · N5512 · Lkheed 188A · Wing, Plate/Skin
  > YIP - LEFT DRY BAY, UPPER SURFACE, CRACK INDICATION COMING FROM UNDER FASTENER BETWEEN NR 19 AND 20 RISERS AT LT WS 170, CRACK SIZE 1.25 BY.5. CLEANED OUT CRACK PER L-188 SRM 51-2-7 PAGE 2. REPAIRED PER ZANTOP DRAWING L33-R01. (M)
- [SDR ZIAA00008](https://openairdocs.org/sdr/ZIAA00008.md): Panel · cracked · Jul 27, 2000 · N5512 · Lkheed 188A · Wing, Plate/Skin
  > YIP - LEFT DRY BAY, UPPER SURFACE, CRACK INDICATION IN FORWARD RADIUS OF NR 19 RISER AT LT WS 170, CRACK SIZE 1X.375. CLEANED OUT CRACK PER L-188 SRM 51-2-7 PAGE 2. REPAIRED PER ZANTOP DWG L33-R01. (M)
- [SDR ZIAA00007](https://openairdocs.org/sdr/ZIAA00007.md): Panel · cracked · Jul 27, 2000 · N5512 · Lkheed 188A · Wing, Plate/Skin
  > YIP - LEFT DRY BAY, UPPER SURFACE, CRACK INDICATION COMING FROM UNDER FASTENER BETWEEN NR 17-18 RISERS AT LT WS 170, CRACK SIZE.75 INCH BY.375. CLEANED OUT CRACK PER L-188 SRM 51-2-7 PAGE 2. REPAIRED PER ZANTOP DWG L33-R01. (M)
- [SDR ZIAA01001](https://openairdocs.org/sdr/ZIAA01001.md): Generator · failed · Apr 26, 2000 · N346HA · Lkheed 188A · AC Generator-Alternator
  > YIP - SHUTDOWN ENGINE BECAUSE OF GENERATOR DISENGAGE LIGHT. REMOVED AND REPLACED NR 1 GENERATOR IAW N24-10. (M)
- [SDR ZIAA00005](https://openairdocs.org/sdr/ZIAA00005.md): Panel · cracked · Feb 25, 2000 · N5522 · Lkheed 188A · Wing, Plate/Skin
  > YIP - CRACK IND NR 1 UPPER RISER FORWARD RADIUS AT APPROX LWS 197, DRY BAY, EIGHT INCH CRACK. REPAIRED RISER NR 1 PER ZANTOP DWG K41-R02. (M)
- [SDR ZIAA00004](https://openairdocs.org/sdr/ZIAA00004.md): Panel · cracked · Feb 25, 2000 · N5522 · Lkheed 188A · Wing, Plate/Skin
  > YIP - CRACK BETWEEN RISERS 19 AND 20, UPPER PLANK AT LWS 209. REPAIRED PER SB675 LOCKHEED DWG 842362. (M)
- [SDR ZIAA00003](https://openairdocs.org/sdr/ZIAA00003.md): Panel · cracked · Feb 15, 2000 · N5522 · Lkheed 188A · Wing, Plate/Skin
  > YIP - CRACK IN RADIUS OF NR 14 RISER, APPROX RWS 205 UPPER SURFACE, DRY BAY. REPAIRED RISER NR 14 PER ZANTOP DWG K41-R01. (M)
- [SDR ZIAA00002](https://openairdocs.org/sdr/ZIAA00002.md): Skin · corroded · Feb 7, 2000 · N5522 · Lkheed 188A · Fuselage Main, Plate/Skin
  > YIP - RIGHT LOWER FUSELAGE, FORWARD OF WING FRONT BEAM CORRODED, FS 552-565. REMOVED CORRODED SECTION OF FUSELAGE SKIN. REPAIRED FUSELAGE SKIN AS PER L-188 SRM REF 53-2-1 FIG 2 SHEET 3. (M)
- [SDR ZIAA98040](https://openairdocs.org/sdr/ZIAA98040.md): Fire Loop · malfunctioned · Oct 23, 1998 · N5512 · Lkheed 188A · Fire Detection
  > MEM - SHUTDOWN NR 4 ENGINE DUE TO FIRE WARNING IN ZONES 2/3 AT 1811Z. FIRED BOTTLE AND LIGHTS WENT OUT. AT 1838Z FIRE WARNING IN ZONES 2/3, ENGINE NR 4 CAME ON AGAIN. FIRED SECOND BOTTLE AND WARNING REMAINED ON. DIVERTED TO MEM. REMOVED AND REPLACED NR 3/
- [SDR ZIAA98032](https://openairdocs.org/sdr/ZIAA98032.md): Panel · cracked · Aug 18, 1998 · N346HA · Lkheed 188A · Wing, Plate/Skin
  > YIP - PER AD 66-04-02 INSPECTION, LEFT WING LOWER SURFACE DRY BAY, 2 INCH LONG SUBSRUFACE RP/UT CORROSION/CRACK INDICATION IN PLANK 3 AT 2/3 PLANK JOINT, LWS 166-168. ROUTED OUT CRACKED AREA, LWS164 TO LWS168, PER SB620. FABRICATED AND INSTALLED REPAIR PER S
- [SDR ZIAA98031](https://openairdocs.org/sdr/ZIAA98031.md): Panel · cracked · Aug 18, 1998 · N346HA · Lkheed 188A · Wing, Plate/Skin
  > YIP - PER AD 66-04-02 INSPECTION, LT WING UPPER SURFACE-DRY BAY, 7 INCH LONG SUBSURFACE RP/UT CORROSION/CRACK INDICATION IN PLANK 2 AT 2/3 PLANK JOINT, LWS 172-179. ROUTED OUT CRACKED AREA, LWS 176 TO LWS 180, PER SB 620. REPAIRED PER ZIA DRAWING F25-R07. (
- [SDR ZIAA98030](https://openairdocs.org/sdr/ZIAA98030.md): Panel · cracked · Aug 18, 1998 · N346HA · Lkheed 188A · Wing, Plate/Skin
  > YIP - PER AD 66-04-02 INSPECTION, LEFT WING UPPER SURFACE-DRY BAY. 5 INCH LONG SUBSURFACE RP/UT CORROSION/CRACK INDICATION IN PLANK 7 AT 6/7 PLANK JOINT, LWS 188-193. ROUTED OUT CRACKED AREA, LWS 188.5 TO LWS197.5, PER SB 620. FABRICATED AND INSTALLED REPAI
- [SDR ZIAA98029](https://openairdocs.org/sdr/ZIAA98029.md): Panel · cracked · Aug 18, 1998 · N346HA · Lkheed 188A · Wing, Plate/Skin
  > YIP - PER AD 66-04-02 INSPECTION, LEFT WING UPPER SURFACE-DRY BAY. 2 INCH LONG SUBSURFACE RP/UT CORROSION/CRACK INDICATION IN PLANK 1 AT 1/2 PLANK JOINT, LWS 181-183. ROUTED OUT CRACKED AREA, LWS176.5 TO LWS180.5, PER SB620. REPAIRED PER ZIA DRAWING F25-R07
- [SDR ZIAA98028](https://openairdocs.org/sdr/ZIAA98028.md): Panel · cracked · Aug 18, 1998 · N346HA · Lkheed 188A · Wing, Plate/Skin
  > YIP - PER AD 66-04-02 INSPECTION, LEFT WING UPPER SURFACE-DRY BAY. 2 INCH LONG SUBSURFACE RP/UT CORROSION/CRACK INDICATION IN PLANK 1 AT 1/2 PLANK JOINT, LWS 196-198. ROUTED OUT CRACKED AREA, LWS194 TO LWS196.5, PER SB620. REPAIRED PER ZIA DRAWING F25-R07.
- [SDR ZIAA98027](https://openairdocs.org/sdr/ZIAA98027.md): Panel · cracked · Aug 18, 1998 · N346HA · Lkheed 188A · Wing, Plate/Skin
  > YIP - PER AD 66-04-02 INSPECTION, LEFT WING NR 2 FUEL TANK-LOWER SURFACE. 2 INCH LONG SUBSURFACE RP/UT CORROSION/CRACK INDICATION IN PLANK 4 AT 3/4 PLANK JOINT, LWS 115-117. ROUTED OUT CRACKED AREA, LWS115 TO LWS119, PER SB620. REPAIRED PER ZIA DRAWING F25-
- [SDR ZIAA98038](https://openairdocs.org/sdr/ZIAA98038.md): Panel · cracked · Aug 17, 1998 · N346HA · Lkheed 188A · Wing, Plate/Skin
  > YIP - PER AD 66-04-02 INSPECTION, LEFT WING NR 2 FUEL TANK UPPER SURFACE. THREE INCH LONG SUBSURFACE RP/UT CORROSION/CRACK INDICATION IN PLANK 9 AT 8/9 JOINT, LWS 88-91. ROUTED OUT CRACKED AREA, WS 87 TO WS 90 PER SB620. INSTALLED REPAIR PER SB620 DRAWING 8

Next page: https://openairdocs.org/model/cessna-188a/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 aircraft_model_key = '188A'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/cessna-188a/reports

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