# Service difficulty reports: Boeing 737-2H5

A list on [Boeing 737-2H5](https://openairdocs.org/model/boeing-737-2h5.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 81 reports

- [SDR 99ZZZM403](https://openairdocs.org/sdr/99ZZZM403.md): Engine · lost power · May 17, 1999 · N220US · Boeing 7372H5 · Engine (Turbine/Turboprop)
  > DURING TAKEOFF AT 80-90 KNOTS, NR 2 ENGINE LOST POWER, WAS SHUTDOWN AND TAKEOFF ABORTED. CAUSE UNDER INVESTIGATION AS TO FOD INGESTION OR NOT. (M)
- [SDR 98ZZZX3002](https://openairdocs.org/sdr/98ZZZX3002.md): Turbine · failed · Jul 28, 1998 · N220US · Boeing 7372H5 · Turbine Section
  > ON TAKEOFF FROM GSO ON FLT 405 AT 500 FEET AGL, THE NR 1 ENGINE SHUT DOWN DUE TO APPARENT LPT FAILURE. THE TURBINE WAS CONTAINED AND NO FIRE OR OTHER DAMAGE OCCURRED. THE FLIGHT CREW CONTINUED TO 2,000 FEET, DECLARED EMERGENCY TO GSO TOWER, WAS CLEARED VISUA
- [SDR 98ZZZX2562](https://openairdocs.org/sdr/98ZZZX2562.md): Flashlight · failed · Jul 2, 1998 · N220US · Boeing 7372H5 · Emergency Lighting
  > DURING PRE-FLIGHT CHECK, THE F/A REPORTED THAT ONE OF THE 2 FLASHLIGHTS IN THE AFT GALLEY DID NOT BLINK WITHIN THE REQUIRED 7 SECONDS. PLACED FLASHLIGHT ON MEL 25-12.
- [SDR 98ZZZM494](https://openairdocs.org/sdr/98ZZZM494.md): Power Supply · inoperative · May 27, 1998 · N221US · Boeing 7372H5 · Emergency Lighting
  > FORWARD LEFT (PAX) AND RT SERVICE DOOR EXIT EMERGENCY LIGHTS INOP. REMOVED AND REPLACED FORWARD EMERGENCY LIGHTS POWER SUPPLY PACK, S/N ON 1715, S/N OFF 15002, P/N 60-1321-1, IAW MM 33-51-71. (M)
- [SDR 98ZZZM496](https://openairdocs.org/sdr/98ZZZM496.md): Wire · chafed · May 22, 1998 · N220US · Boeing 7372H5 · Light System Wiring
  > EMERGENCY EXIT LIGHT PATH INOP. REPAIRED BROKEN WIRE UNDER SEAT 2ABC. (M)
- [SDR 98ZZZM495](https://openairdocs.org/sdr/98ZZZM495.md): Bulb · failed · May 22, 1998 · N220US · Boeing 7372H5 · Emergency Lighting
  > FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BULB. (M)
- [SDR 98ZZZM401](https://openairdocs.org/sdr/98ZZZM401.md): Splice · broken · Feb 26, 1998 · N221US · Boeing 7372H5 · Emergency Lighting
  > ON OVERNIGHT CHECK, FOUND ROW 2 EMERGENCY LIGHT INOP. FOUND BUTT SPLICE BROKEN. REINSTALLED NEW SPLICE, OPS CHECK OK. (M)
- [SDR 98ZZZX1075](https://openairdocs.org/sdr/98ZZZX1075.md): Hydraulic Tube · chafed · Feb 13, 1998 · N220US · Boeing 7372H5 · Hydraulic System, Main
  > FLT 992/23 NCO - LOST A-HYDRAULIC SYSTEM PRESSURE AND QUANTITY AFTER TAKEOFF CLIMBING THROUGH APPROX 3,500 FEET. COMPLETED EMERGENCY CHECK LIST. BURNED OFF EXCESS FUEL AND LANDED WITH AIRCRAFT WEIGHT AT 96,100 POUNDS. GEAR PINS INSTALLED FOR TOWING. INSPEC
- [SDR 98ZZZX900](https://openairdocs.org/sdr/98ZZZX900.md): Stator · damaged · Feb 4, 1998 · N220US · Boeing 7372H5 · Compressor Bleed Control
  > DURING B-CHECK, NR 2 ENGINE INSPECTION FOUND FIRST STAGE COMPRESSOR STATOR VANE DAMAGE. ONE VANE HAD RIVETS SHEARED, VANE SHIFTED AND CAUSED DAMAGE TO ADJACENT VANE. REPLACED 1ST STAGE COMPRESSOR STATOR ASSY ON WING PER MM 72-00-21, 72-00-23, AND 72-00-33.
- [SDR 98ZZZX902](https://openairdocs.org/sdr/98ZZZX902.md): Power Supply · inoperative · Jan 25, 1998 · N220US · Boeing 7372H5 · Emergency Lighting
  > INTERIOR AND EXTERIOR EMERGENCY LIGHTS AT FORWARD ENTRY AND FORWARD SERVICE DOORS DO NOT ILLUMINATE. FOUND ON RON SVC CHECK. REPLACED EMERGENCY LIGHT BATTERY AND POWER SUPPLY IAW B737 MM 33-50. OPERATIONAL CHECKS OK. REF: OPERATOR CONTROL NR 98ZZZX901.
- [SDR 98ZZZX901](https://openairdocs.org/sdr/98ZZZX901.md): Battery · discharged · Jan 25, 1998 · N220US · Boeing 7372H5 · Emergency Lighting
  > INTERIOR AND EXTERIOR EMERGENCY LIGHTS AT FORWARD ENTRY AND FORWARD SERVICE DOORS DO NOT ILLUMINATE. FOUND ON RON SVC CHECK. REPLACED EMERGENCY LIGHT BATTERY AND POWER SUPPLY IAW B737 MM 33-50. OPERATIONAL CHECKS OK. REF: OPERATOR CONTROL NR 98ZZZX902.
- [SDR 98ZZZM80](https://openairdocs.org/sdr/98ZZZM80.md): Light · inoperative · Dec 12, 1997 · N221US · Boeing 7372H5 · Emergency Lighting
  > FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT INOP, FOUND ON RON MAINTENANCE CHECK. REPLACED LIGHT ASSY, OPS CHECK GOOD. (M)
- [SDR 98ZZZM79](https://openairdocs.org/sdr/98ZZZM79.md): Light · damaged · Dec 10, 1997 · N220US · Boeing 7372H5 · Emergency Lighting
  > L2 DOOR EMERGENCY EXITLIGHT DAMAGED DURING REAR STAIR EXTENSION DURING TRAINING EXCERISE. UNIT WAS REPLACED WITH FLT COMPT EMERGENCY EXIT LIGHT, DUE PART NIS. FLT COMPT EMERGENCY EXIT LIGHT WAS MEL'D. AIRCRAFT RELEASED PER MEL 33-15 AND FLT COMPT. EMERGENC
- [SDR 97ZZZM1069](https://openairdocs.org/sdr/97ZZZM1069.md): Tab Hinge · worn · Sep 11, 1997 · N220US · Boeing 7372H5 · Elevator Tab, Attach Fittings
  > VIBRATION FELT IN CONTROL YOKE AS WELL AS THROUGHOUT THE AIRCRAFT F/A'S STATE VIBRATION WAS MORE PROMINENT IN AFT OF AIRCRAFT, MORE PROMINENT ON RIGHT SIDE. INSPECTED AND FOUND INBOARD TAB BEARING BLOCK AND FWD HINGE BRACKET WORN, PER MM 27-31-31A. INSPECTED
- [SDR 97ZZZX2605](https://openairdocs.org/sdr/97ZZZX2605.md): Power Supply · inoperative · May 7, 1997 · N220US · Boeing 7372H5 · Emergency Lighting
  > ON ROUTINE CHECK, OVERNIGHT INSPECTION, MAINTENANCE REPORTED AFT SERVICE DOOR EMERGENCY LIGHT INOPERABLE. REPLACED POWER SUPPLY.
- [SDR 97ZZZM426](https://openairdocs.org/sdr/97ZZZM426.md): Skin · cracked · Mar 2, 1997 · N221US · Boeing 7372H5 · Fuselage Main, Plate/Skin
  > FOUND 5 CRACKS AT FASTENERS STATION 373, 374, 375, 377, STRINGER 15L. REPAIRED PER SRM 53-30-3. (M)
- [SDR 97ZZZM425](https://openairdocs.org/sdr/97ZZZM425.md): Skin · cracked · Mar 2, 1997 · N221US · Boeing 7372H5 · Fuselage Main, Plate/Skin
  > FOUND.125 INCH CRACK AT FASTENER HOLE. REPAIRED PER SRM 53-30-1.
- [SDR 97ZZZM424](https://openairdocs.org/sdr/97ZZZM424.md): Skin · cracked · Mar 2, 1997 · N221US · Boeing 7372H5 · Fuselage Main, Plate/Skin
  > FOUND TWO.25 INCH LONG CRACKS. REPAIRED PER SRM 53-30-3 FIG 1.
- [SDR 97ZZZM423](https://openairdocs.org/sdr/97ZZZM423.md): Skin · cracked · Mar 2, 1997 · N221US · Boeing 7372H5 · Fuselage Main, Plate/Skin
  > FOUND TWO CRACKS AT FASTENER HOLES. REPAIRED PER SRM 53-30-3.
- [SDR 97ZZZM422](https://openairdocs.org/sdr/97ZZZM422.md): Frame · cracked · Mar 2, 1997 · N221US · Boeing 7372H5 · Fuselage Main, Frame
  > FOUND ONE INCH CRACK IN FRAME. REPAIRED PER SRM 51-40-2.
- [SDR 97ZZZM421](https://openairdocs.org/sdr/97ZZZM421.md): Frame · cracked · Mar 2, 1997 · N221US · Boeing 7372H5 · Fuselage Main, Frame
  > LEFT OUTBOARD CHORD ANGLE CRACKED STATION 1156 WL 274,.75 INCH CRACK. REPAIRED PER EO 5391G569.
- [SDR 97ZZZM420](https://openairdocs.org/sdr/97ZZZM420.md): Stringer · cracked · Mar 2, 1997 · N221US · Boeing 7372H5 · Fuselage Main, Longeron/Stringer
  > ONE INCH CRACK IN STRINGER. REPAIRED PER SRM 53-10-3.
- [SDR 97ZZZM419](https://openairdocs.org/sdr/97ZZZM419.md): Skin · disbond · Mar 2, 1997 · N221US · Boeing 7372H5 · Fuselage Main, Plate/Skin
  > SKIN DISBONDED AT LOWER CORNERS OF EMERGENCY EXIT APERTURE, REPAIRED PER EA 42068.
- [SDR 97ZZZM418](https://openairdocs.org/sdr/97ZZZM418.md): Skin · cracked · Mar 2, 1997 · N221US · Boeing 7372H5 · Fuselage Main, Plate/Skin
  > 3 INCH BY 5 INCH DELAMINATED AREA AND CRACKS AT SIX FASTENER HOLES. REPAIRED PER EA 42062. (M)
- [SDR 97ZZZM417](https://openairdocs.org/sdr/97ZZZM417.md): Bulkhead Fitting · cracked · Mar 2, 1997 · N221US · Boeing 7372H5 · Fuselage Main, Bulkhead
  > BULKHEAD FITTING CRACKED 3 INCHES. TIME LIMITED REPAIR INSTALLED PER EA 42071 AND DWG 65C 29229. (M)
- [SDR 97ZZZM245](https://openairdocs.org/sdr/97ZZZM245.md): Skin · corrosion · Jan 27, 1997 · N220US · Boeing 7372H5 · Fuselage Main, Plate/Skin
  > CLT - INSPECTION VISUALLY AND BY NDT/HFEC FOUND CORRODED AREA MEASURING APPROX 15 INCHES BY 20 INCH LOCATED AT FUSELAGE BS 312, STRINGER 27R AND BEAR STRAP AND E-E CUTOUT. INSPECTION CARD NR J 2C-50-9012. INSTALLED TRIPLER, FILLER AND SKIN REPAIR AS PER EA N
- [SDR 97ZZZM244](https://openairdocs.org/sdr/97ZZZM244.md): Stringer · corrosion · Jan 27, 1997 · N220US · Boeing 7372H5 · Fuselage Main, Longeron/Stringer
  > CLT - INSPECTION VISUALLY, FOUND CORROSION APPROXIMATELY 14 INCH BY 20 INCH LOCATED AT BS 344, STRINGER 27R-28R. INSPECTION CARD NR J2C-40-5325-1, SSID/SIP REF NR SSI F-9. REPLACED INTERNAL BEAM CHORD SECTION AT BS 351, RBL 15.47. INSTALLED DOUBLER, EXTERNA
- [SDR 97ZZZM23](https://openairdocs.org/sdr/97ZZZM23.md): Connector · shorted · Dec 5, 1996 · N220US · Boeing 7372H5 · Fire Detection
  > NR 1 ENGINE FIRE WARNING CAME ON INTERMITTENTLY ON LANDING. FOUND DEFECTIVE CANNON PLUG, MANUFACTURERS PART NR 42839 KS 14S-5SX SHORTED.
- [SDR 96ZZZX2793](https://openairdocs.org/sdr/96ZZZX2793.md): Skin · cracked · Apr 30, 1996 · N220US · Boeing 7372H5 · Fuselage Main, Plate/Skin
  > GSO - VISUAL INSPECTION FOUND.9 INCH CRACK IN OUTER SKIN AT FS 767, STR 19R DURING WALK-AROUND. INSTALLED DOUBLER USING BLIND FASTENERS (OM-7 32938), PER SRM 53-30-3, FIGURE 6.
- [SDR 96ZZZX1484](https://openairdocs.org/sdr/96ZZZX1484.md): Skin · cracked · Mar 1, 1996 · N221US · Boeing 7372H5 · Fuselage Main, Plate/Skin
  > GSO -.1250 INCH CRACK AT RIVET HOLE FOUND. INSTALLED DOUBLER SRM 53-30-3, FIGURE 6.
- [SDR 96ZZZX1483](https://openairdocs.org/sdr/96ZZZX1483.md): Skin · cracked · Mar 1, 1996 · N221US · Boeing 7372H5 · Fuselage Main, Plate/Skin
  > GSO - FIVE.25 INCH CRACKS AT RIVET HOLES FOUND. INSTALLED REPAIR PER E.A. 40951.
- [SDR 96ZZZX1482](https://openairdocs.org/sdr/96ZZZX1482.md): Skin · cracked · Mar 1, 1996 · N221US · Boeing 7372H5 · Fuselage Main, Plate/Skin
  > GSO - 3 CRACKS FORWARD UPPER CORNER, FORWARD SERVICE DOORWAY. INSTALLED DOUBLER PER E.A. 40950.
- [SDR E9WA](https://openairdocs.org/sdr/E9WA.md): Skin · damaged · Feb 16, 1996 · N221US · Boeing 7372H5 · Vertical Stabilizer, Plate/Skin
  > CLT - INSPECTION VISUALLY FOUND MISSING TRAILING EDGE HONEYCOMB CORE MATERIAL LOCATED AT THE VERTICAL STAB AT RUDDER STATION 218 RIGHT TRAILING EDGE PANEL. COMPOSITE REPAIRED AS PER BOEING SRM 51-40-13. (M)
- [SDR 96ZZZM798](https://openairdocs.org/sdr/96ZZZM798.md): Skin · damaged · Feb 16, 1996 · N221US · Boeing 7372H5 · Fuselage Main, Plate/Skin
  > CLT - INSPECTION FOUND 2 PREVIOUSLY INSTALLED DOUBLERS WITH BLIND FASTENERS LOCATED AT FUSELGE SKIN, FS 727A AT STRINGER 15R AND 16R. INSTALLED EXTERNAL DOUBLER AS PER BOEING SRM 53-30-3 FIG 6 AND USAIR EA NR 24906. (M)
- [SDR 96ZZZM744](https://openairdocs.org/sdr/96ZZZM744.md): Skin · disbond · Feb 16, 1996 · N221US · Boeing 7372H5 · Fuselage Main, Plate/Skin
  > CLT - INSPECTION BY ULTRASONIC, FOUND SKIN AND DOUBLER DISBOND MEASURING 12 INCHES BY 2.5 INCHES LOCATED FUSELAGE SKIN AT STATION 927-947 AND STRINGER 14L. INSTALLED FIELD FASTENERS AS PER SRM 53-30-3 FIG 17 DETAIL 1. (M)
- [SDR 96ZZZM743](https://openairdocs.org/sdr/96ZZZM743.md): Skin · cracked · Feb 16, 1996 · N221US · Boeing 7372H5 · Fuselage Main, Plate/Skin
  > CLT - INSPECTION VISUALLY FOUND A CRACK THROUGH RIVET.1875 INCH UP AND.125 INCH DOWN LOCATED AT FUSELAGE SKIN AT STATION 251 AND STRINGER 11L. INSTALLED DOUBLER AS PER BOEING SRM 53-30-03 AND USAIR EO NR 22870. (M)
- [SDR 96ZZZM742](https://openairdocs.org/sdr/96ZZZM742.md): Skin · disbond · Feb 16, 1996 · N221US · Boeing 7372H5 · Fuselage Main, Plate/Skin
  > CLT - INSPECTION BY ULTRASONIC, FOUND DISBONDED SKIN AND DOUBLER MEASURING 9 INCHES BY 5 INCHES LOCATED AT THE FUSELAGE SKIN AT STATION 288, STRINGER 14L AND STRINGER 15L. INSTALLED FIELD DOUBLERS AS PER BOEING SRM 53-30-3 DETAIL 1 FIG 17. (M)
- [SDR 96ZZZM741](https://openairdocs.org/sdr/96ZZZM741.md): Skin · disbond · Feb 16, 1996 · N221US · Boeing 7372H5 · Fuselage Main, Plate/Skin
  > CLT - INSPECTION BY ULTRASONIC, FOUND DISBONDED SKIN AND DOUBLER AT THE FUSELAGE SKIN MEASURING 5 INCHES BY 18 INCHES LOCATED AT STATION 920 TO 927 AND STRINGER 9R TO STRINGER 10R. INSTALLED FIELD RIVETS AS PER BOEING SRM 53-30-3. (M)
- [SDR 96ZZZM740](https://openairdocs.org/sdr/96ZZZM740.md): Skin · disbond · Feb 16, 1996 · N221US · Boeing 7372H5 · Fuselage Main, Plate/Skin
  > CLT - INSPECTION BY ULTRASONIC, FOUND SKIN AND DOUBLER DISBOND LOCATED AT FUSELAGE SKIN MEASURING 3 INCHES BY 4 INCHES AT STATION 967 ABOVE STRINGER 5L. INSTALLED FIELD RIVETS AS PER SRM 53-30-3 FIG 17. (M)
- [SDR 96ZZZM739](https://openairdocs.org/sdr/96ZZZM739.md): Skin · disbond · Feb 16, 1996 · N221US · Boeing 7372H5 · Fuselage Main, Plate/Skin
  > CLT - INSPECTION BY ULTRASONIC, FOUND SKIN AND DOUBLER DISBOND LOCATED AT FUSELAGE SKIN MEASURING 5 INCHES BY 4 INCHES AT STATION 356, STRINGER 15L AND 16L. INSTALLED FIELD FASTENERS AS PER BOEING SRM 53-30-3 DETAIL I AND TABLE III FIG 17. (M)
- [SDR 96ZZZM738](https://openairdocs.org/sdr/96ZZZM738.md): Skin · disbond · Feb 16, 1996 · N221US · Boeing 7372H5 · Fuselage Main, Plate/Skin
  > CLT - INSPECTION BY ULTRASONIC, FOUND SKIN AND DOUBLER DISBOND LOCATED AT FUSELAGE SKIN MEASURING 14 INCHES BY 2.5 INCHES AT STATION 902 TO 914 AND STRINGER 13R TO STRINGER 14R. INSTALLED FIELD RIVETS AS PER BOEING SRM 53-30-3. (M)
- [SDR 96ZZZM737](https://openairdocs.org/sdr/96ZZZM737.md): Skin · cracked · Feb 16, 1996 · N221US · Boeing 7372H5 · Fuselage Main, Plate/Skin
  > CLT - INSPECTION VISUALLY FOUND AND VERIFIED WITH HFEC A 1.25 INCH CRACK LOCATED AT FUSELAGE SKIN FS 1137 AND STRINGER 12L. INSTALLED DOUBLER AS PER BOEING SRM 53-30-3 FIG 30. (M)
- [SDR 96ZZZM736](https://openairdocs.org/sdr/96ZZZM736.md): Support Beam · corrosion · Feb 16, 1996 · N221US · Boeing 7372H5 · Fuselage Miscellaneous Structure
  > CLT - INSPECTION VISUALLY FOUND LEVEL I CORROSION AT THE FUSELAGE FLOOR SUPPORT BEAM LOCATED AT LBL 2 TO LBL 6 AND STATION 1014. FABRICATED REPLACEMENT H-CHANNEL AND ATTACH ANGLE AS PER BOEING SRM 51-00-02. (M)
- [SDR 96ZZZM735](https://openairdocs.org/sdr/96ZZZM735.md): Skin · gouged · Feb 16, 1996 · N221US · Boeing 7372H5 · Fuselage Main, Plate/Skin
  > CLT - INSPECTION VISUALLY FOUND A 1.5 INCH GOUGE.019 DEEP AT FUSELAGE SKIN LOCATED AT FS 360 1 INCH ABOVE STRINGER 18L. INSTALLED DOUBLER AS PER BOEING SRM 53-30-3, FIG 28. (M)
- [SDR 96ZZZM734](https://openairdocs.org/sdr/96ZZZM734.md): Skin · disbond · Feb 16, 1996 · N221US · Boeing 7372H5 · Fuselage Main, Plate/Skin
  > CLT - INSPECTION BY ULTRASONIC FOUND DISBONDED SKIN AND DOUBLER AT THE FUSELAGE SKIN LOCATED AT STATION 927 TO 947 AND STRINGER 21R TO STRINGER 20R. REMOVED AND REPLACED SKIN DOUBLER AS PER BOEING SRM 53-30-3 FIG 17. (M)
- [SDR 96ZZZM733](https://openairdocs.org/sdr/96ZZZM733.md): Skin · corrosion · Feb 16, 1996 · N221US · Boeing 7372H5 · Fuselage Main, Plate/Skin
  > CLT - INSPECTION VISUALLY FOUND A LEVEL I CORRODED PRODUCTION STRINGER SPLICE 6 INCHES AT THE FUSELAGE SKIN LOCATED AT STATION 908 AND STRINGER 20R. REPLACED AND REPAIR STRINGER PRODUCTION SPLICE AS PER BOEING SRM 51-00-00. (M)
- [SDR 96ZZZM732](https://openairdocs.org/sdr/96ZZZM732.md): Skin · disbonded · Feb 16, 1996 · N221US · Boeing 7372H5 · Fuselage Main, Plate/Skin
  > CLT - INSPECTION VISUALLY FOUND 6 INCH DISBONDED FUSELAGE SKIN LOCATED AT STATION 954 BETWEEN STRINGER 24 AND STRINGER 23R. REPLACED SKIN AS PER USAIR EA NR 58009 AND JOB CARD JZ-57-53500 C-1. (M)
- [SDR 96ZZZM731](https://openairdocs.org/sdr/96ZZZM731.md): Angle · cracked · Feb 16, 1996 · N221US · Boeing 7372H5 · Fuselage Miscellaneous Structure
  > CLT - INSPECTION VISUALLY FOUND A 1.5 INCH CRACK LOCATED AT THE FUSELAGE RADIUS OF ANGLE AT FS 1085 AND STRINGER 2L. INSTALLED AND MANUFACTURED ANGLE AS PER BOEING SRM 20-30-06. (M)
- [SDR 96ZZZM730](https://openairdocs.org/sdr/96ZZZM730.md): Skin · disbond · Feb 16, 1996 · N221US · Boeing 7372H5 · Fuselage Main, Plate/Skin
  > CLT - INSPECTION BY ULTRASONIC, FOUND TWO 6 INCHES BY 6 INCHES AND 8 INCHES BY 2 INCHES AREAS OF SKIN AND DOUBLER DISBOND LOCATED AT THE FUSELAGE SKIN BETWEEN STATION 277 AND 294.5, STRINGER 5R AND STRINGER 8R. INSTALLED FIELD FASTENERS AS PER BOEING SRM 53-3
- [SDR 96ZZZM729](https://openairdocs.org/sdr/96ZZZM729.md): Skin · disbonded · Feb 16, 1996 · N221US · Boeing 7372H5 · Fuselage Main, Plate/Skin
  > CLT - INSPECTION BY ULTRASONIC, FOUND FUSELAGE SKIN AND DOUBLER DISBOND LOCATED AT STATION 927 TO 947, STRINGER 9L AND STRINGER 10L. INSTALLED FIELD DOUBLERS AS PER BOEING SRM 53-30-3 FIG 17. (M)

Next page: https://openairdocs.org/model/boeing-737-2h5/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 = '7372H5'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-737-2h5/reports

---
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