# Service difficulty reports: Boeing 737 2J8

A list on [Boeing 737 2J8](https://openairdocs.org/model/boeing-737-2j8.md).

Newest first. General aviation reporting is voluntary.

- [SDR DL73E010722](https://openairdocs.org/sdr/DL73E010722.md): Support Fitting · corroded · May 5, 2001 · N235WA · Boeing 7372J8 · Fuselage, Landing Gear Attach Fittings
  > THE WL 188.5 LUG ON THE LT MLG SIDE STRUT SUPPORT FITTING AT FS 685 WAS FOUND WITH CORROSION IN THE LUG BORE. THE CORROSION WAS REMOVED BY OVERSIZING THE LUG BORE. AN ALUMINUM REPAIR BUSHING WAS INSTALLED TO RESTORE THE LUG DIAMETER PER ER/A 380741-14.
- [SDR DL73E010721](https://openairdocs.org/sdr/DL73E010721.md): Skin · cracked · May 5, 2001 · N235WA · Boeing 7372J8 · Fuselage Main, Plate/Skin
  > A 1.2 INCH LONG CRACK WAS FOUND IN THE BONDED SKIN ASSY AT THE LOWER FWD CORNER OF THE AFT GALLEY DOOR CUTOUT. THE CRACK WAS REMOVED WITH A CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER AND TRIPLER PER ER/A 380732-14, REV B
- [SDR DL73E010723](https://openairdocs.org/sdr/DL73E010723.md): Skin · cracked · May 4, 2001 · N235WA · Boeing 7372J8 · Fuselage Main, Plate/Skin
  > A TYPICAL CRACK WAS FOUND IN THE LOWER FORWARD CORNER OF THE AFT ENTRY DOOR CUTOUT. THE CRACK WAS IN THE BONDED SKIN ASSY AND THE UNDERLYING BEAR STRAP. THE CRACK WAS REMOVED WITH A 2.5 X 1 INCH CUTOUT. THE AREA WAS REPAIRED WITH THREE EXTERNAL ALUMINUM DO
- [SDR DL73E002241](https://openairdocs.org/sdr/DL73E002241.md): Floorbeam · cracked · Nov 14, 2000 · N235WA · Boeing 7372J8 · Fuselage Main, Floor Beam
  > THE UPPER CAP OF THE BL 0.07 LONGITUDINAL FLOORBEAM WAS FOUND WITH CRACKS COMMON TO THE FLOOR PANEL ATTACH HOLES BETWEEN FS 660 & 664. THE CRACKS ARE TYPICAL OF BAC S/B 737-57-1210. THE CAP CRACKS WERE REPAIRED WITH ALUMINUM REPAIR ANGLES PER THE S/B AND PER
- [SDR DL73E002068](https://openairdocs.org/sdr/DL73E002068.md): Switch · malfunctioned · Oct 19, 2000 · N235WA · Boeing 7372J8 · Central Warning
  > AS POWER WAS PUSHED UP FOR TAKEOFF ABOVE 1.4 EPR TAKEOFF WARNING HORN SOUNDED INTERMITTENT TONE. TAKEOFF WAS DISCONTINUED AT AROUND 20 - 30 KTS. A CHECK SHOWED AIRCRAFT CONFIGURATION PERFECTLY NORMAL, FLAPS 5, SPEEDBRAKE DOWN, TRIM 5.0 ETC. AFTER DEPARTING
- [SDR DL73E000209](https://openairdocs.org/sdr/DL73E000209.md): Skin · cracked · Jan 27, 2000 · N235WA · Boeing 7372J8 · Fuselage Main, Plate/Skin
  > THE LOWER AFT CORNER OF THE R1 DOOR CUTOUT WAS FOUND WITH A 1.75 INCH TYPICAL CRACK IN THE SKIN AND BONDED DOUBLER AND A 1.5 INCH CRACK IN THE UNDERLYING BEAR STRAP. THE CRACK WAS ROUTED OUT OF THE SKIN STACK UP AND REPAIRED WITH 3 EXTERNAL ALUMINUM DO
- [SDR DL73E991054](https://openairdocs.org/sdr/DL73E991054.md): Overheat Det · inoperative · May 13, 1999 · N235WA · Boeing 7372J8 · Overheat Detection
  > APU LIGHT ILLUMINATED ON T/O. PULLED HANDLE, LIGHT CONTINUED TO ILLUMINATE ON TAXI BACK. REJECTED TAKEOFF. REPLACED APU TAILPIPE OVERHEAT DET CONNECTOR D1878 AND WIRE W765-451-18R DUE TO HIGH RESISTANCE SHORT. OPS TEST AND RUN TEST CHECK GOOD. CONNECTOR (
- [SDR DL73E990468](https://openairdocs.org/sdr/DL73E990468.md): Light · inop · Mar 5, 1999 · N235WA · Boeing 7372J8 · Emergency Lighting
  > EMERGENCY EXIT LIGHT ABOVE L1 DOOR INOP. REPLACED LIGHT ASSY, OP CKS GOOD.
- [SDR DL73E990249](https://openairdocs.org/sdr/DL73E990249.md): Light · inop · Feb 5, 1999 · N235WA · Boeing 7372J8 · Emergency Lighting
  > EMERGENCY LIGHT ASSY SEAT 12D INOP. REPLACED LIGHT ASSY, TEST GOOD PER MM.
- [SDR DL73E981806](https://openairdocs.org/sdr/DL73E981806.md): Actuator · broken · Sep 1, 1998 · N235WA · Boeing 7372J8 · Drag Control Actuator
  > ON TAXI IN, A-SYS HYD WENT TO ONE GALLON. REPLACED NR 8 SPOILER ACTUATOR.
- [SDR DL73E981407](https://openairdocs.org/sdr/DL73E981407.md): Engine · over temp · Jul 4, 1998 · N235WA · Boeing 7372J8 · Engine (Turbine/Turboprop)
  > ENGINE IN FLIGHT, SHUT DOWN DUE TO OIL TEMP EXCEEDED RED LINE. ENGINE WAS REPLACED.
- [SDR DL73E972306](https://openairdocs.org/sdr/DL73E972306.md): Keel Beam · cracked · Nov 10, 1997 · N235WA · Boeing 7372J8 · Fuselage Main, Keel
  > TWO 1.5 INCH CRACKS FOUND IN THE KEEL BEAM LWR SKIN AT STA 680 AND TWO ADDITIONAL AT STA 696. CRACKS LOCATED AT L/RBL 5. REPAIR PER ERA 363005-14, REV A.
- [SDR DL73E972305](https://openairdocs.org/sdr/DL73E972305.md): Skin · cracked · Nov 10, 1997 · N235WA · Boeing 7372J8 · Fuselage Main, Plate/Skin
  > CRACK FOUND IN THE FUSELAGE SKIN AT STA 727A AND STR 16R. REPAIR PER ERA 330976-14.
- [SDR DL73E972304](https://openairdocs.org/sdr/DL73E972304.md): Skin · cracked · Nov 10, 1997 · N235WA · Boeing 7372J8 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN FOUND WITH A SMALL CRACK IN THE UPPER AFT CORNER OF THE C2 DOOR CUTOUT. REPAIRED PER ERA 330960-14.
- [SDR DL73E972303](https://openairdocs.org/sdr/DL73E972303.md): Structure · corroded · Nov 10, 1997 · N235WA · Boeing 7372J8 · Fuselage Main, Structure
  > SKIN, FRAME AND STRINGERS 27 LT AND RT WERE FOUND WITH CORROSION AT STA 807. REPAIRED PER ERA 330955-14.
- [SDR DL73E972302](https://openairdocs.org/sdr/DL73E972302.md): Frame · cracked · Nov 10, 1997 · N235WA · Boeing 7372J8 · Fuselage Main, Frame
  > R1 DOOR FRAME INTERCOSTAL AT STGR 8A WAS CRACKED IN TYP MANNER SHOWN IN SB 737-53A1108, R5, AT APPROX FS 334. ALSO, THE INTERCOSTAL AT STGR 11 WAS CRACKED. REPAIRED PER SB 737-53A1108, R5.
- [SDR DL73E972301](https://openairdocs.org/sdr/DL73E972301.md): Floorbeam · cracked · Nov 10, 1997 · N235WA · Boeing 7372J8 · Fuselage Main, Floor Beam
  > FLOORBEAM AT FS 520 WAS FOUND CRACKED AT RBL 25 AND LBL 45. REPAIRED PER SB 737-53-1120, R 1.
- [SDR DL73E972112](https://openairdocs.org/sdr/DL73E972112.md): Skin · cracked · Oct 10, 1997 · N235WA · Boeing 7372J8 · Fuselage Main, Plate/Skin
  > THE RT FUSELAGE SKIN BETWEEN FS 747 AND 767 AND S-18R AND S-19R WAS FOUND WITH TWO CRACKS. REPAIRED PER DELTA ER/A 362945-14 AND B737 SRM 53-30-3, FIG 6.
- [SDR DL73E961207](https://openairdocs.org/sdr/DL73E961207.md): Test Module · inoperative · May 18, 1996 · N235WA · Boeing 7372J8 · AC Generation System
  > NR 2 GENERATOR WOULD NOT HOOK UP TO BUS DUE TO NO VOLTAGE. FREQUENCY WAS NORMAL. REPLACED POWER TEST MODULE, OPS CK OK FOR SERVICE.
- [SDR DL73E960757](https://openairdocs.org/sdr/DL73E960757.md): Main Tire · failed · Apr 3, 1996 · N235WA · Boeing 7372J8 · Tire
  > SHORTLY AFTER TAKEOFF, A HYD SYS PRESS FAILED AND QTY WENT TO ZERO. ACCOMPLISHED CHECKLIST AND RETURNED FOR LANDING. AFTER LANDING FOUND NR 3 MAIN TIRE HAD COME APART AND DAMAGED 2 HYDRAULIC LINES. ALSO, TIRE DAMAGED RT WING AND I/B SPOILER ABOVE RT MAIN GE
- [SDR DL73E960715](https://openairdocs.org/sdr/DL73E960715.md): Battery Pack · discharged · Mar 30, 1996 · N235WA · Boeing 7372J8 · Emergency Lighting
  > EMERGENCY PATH LIGHTS BATTERY PACK INOP. REPLACED, CHECKS GOOD.
- [SDR DL73E960741](https://openairdocs.org/sdr/DL73E960741.md): Bulkhead Web · cracked · Mar 29, 1996 · N235WA · Boeing 7372J8 · Fuselage Main, Bulkhead
  > BULKHEAD 178 WAS FOUND CRACKED BENEATH THE VERTICAL STIFFENERS AT LBL 5.7 AND RBL 5.7. DAMAGE REMOVAL RESULTED IN CUT OUTS ON THE LT SIDE 3.5 AND 6 ABOVE WL 195, SAME FOR THE RT SIDE. THE WEB IS MANUFACTURED FROM 0.040 CLAD 2024-T3. ACCOMPLISHED REPAIRS PER
- [SDR DL73E960716](https://openairdocs.org/sdr/DL73E960716.md): Battery Pack · discharged · Mar 27, 1996 · N235WA · Boeing 7372J8 · Emergency Lighting
  > DURING LAYOVER, EMERGENCY LIGHTS FOR OVERWING EMERGENCY EXITS FAILED TEST. REPLACED BATTERY PACK, OPERATION NORMAL.
- [SDR DL73E954725](https://openairdocs.org/sdr/DL73E954725.md): Skin · damaged · Dec 14, 1995 · N235WA · Boeing 7372J8 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS GOUGED BETWEEN FS 380 AND FS 400. THE DAMAGE CUT OUT MEASURES APPROX 4.9 BY 23.1. THE NEWLY DAMAGED SECTION IS BETWEEN 2 PREVIOUSLY DAMAGED SKIN SECTIONS, REPAIRS ACCOMPLISHED PER ER/A'S 230787-14 AND 230789-14. IN ADDITION, AN EXISTIN
- [SDR DL73E950771](https://openairdocs.org/sdr/DL73E950771.md): Frame · cracked · Jan 25, 1995 · N235WA · Boeing 7372J8 · Cargo/Baggage Doors
  > DURING SHOP INSPECTION, A 0.70 INCH CRACK WAS FOUND IN THE INNER RADIUS OF THE FORWARD CARGO DOOR FRAME. THE CRACK IS LOCATED ON THE FORWARD EDGE OF THE DOOR BETWEEN DOOR STOP NR 4 & NR 5. REPAIRED PER ERA 270046-14AD.

## 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 = '7372J8'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-737-2j8/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.