# Service difficulty reports: Boeing 737-448

A list on [Boeing 737-448](https://openairdocs.org/model/boeing-737-448.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 51 reports

- [SDR XV6A2015031100002](https://openairdocs.org/sdr/XV6A2015031100002.md): Repair · unknown · Mar 9, 2015 · N742VA · Boeing 737448 · Standard Practices/Structures
  > REF TECH W/O 1502527. R & R EXISTING REPAIR AT BS 727G IAW DWG 53-15046. EXISTING CATEGORY "C" REPAIR TIME LIMITED REPLACED BY CATEGORY "B" REPAIR.
- [SDR 7AHR201405307372](https://openairdocs.org/sdr/7AHR201405307372.md): Skin · corroded · May 30, 2014 · N742VA · Boeing 737448 · Wing, Plate/Skin
  > RT WING UPPER SKIN AT FRONT SPAR BETWEEN WS475 & WS531 HAS CORROSION. REPAIRED IAW DWG 57-13172-1.
- [SDR 7AHR201405307369](https://openairdocs.org/sdr/7AHR201405307369.md): Skin · corroded · May 30, 2014 · N742VA · Boeing 737448 · Wing, Plate/Skin
  > RIGHT WING UPPER SKIN HAS CORRROSION BETWEEN WS479 & WS505 AT S-11. REPAIRED IAW DWG 57-13169-1.
- [SDR 7AHR201405307374](https://openairdocs.org/sdr/7AHR201405307374.md): Skin · corroded · May 30, 2014 · N742VA · Boeing 737448 · Wing, Plate/Skin
  > RIGHT WING UPPER SKIN AT REAR SPAR AREA HAS CORROSION BETWEEN WS315 & WS370. REPAIRED IAW DWG 57-13174-1.
- [SDR 7AHR201405307373](https://openairdocs.org/sdr/7AHR201405307373.md): Skin · corroded · May 30, 2014 · N742VA · Boeing 737448 · Wing, Plate/Skin
  > RIGHT WING UPPER SKIN HAS CORROSION AT FRONT SPAR BETWEEN WS315 & WS375. REPAIRED IAW DWG 57-13173-1.
- [SDR 7AHR201405307392](https://openairdocs.org/sdr/7AHR201405307392.md): Skin · damaged · May 30, 2014 · N742VA · Boeing 737448 · Wing, Plate/Skin
  > RT WING UPPER SKIN BLENDOUTS BETWEEN WS270 & WS583.
- [SDR 7AHR201405302121](https://openairdocs.org/sdr/7AHR201405302121.md): Skin · damaged · May 30, 2014 · N742VA · Boeing 737448 · Fuselage Main, Plate/Skin
  > AT STRINGER 21 RT BS 360 - 400 EXTERIOR FUSELAGE HAS LARGE CREASE SHOWING IMPRESSION OF FRAME & STRINGER. AREAS WERE FOUND TO BE OUT OF LIMITS IAW SRM 51-00-01. REMOVED DAMAGED AREAS, PERFORMED EDDY CURRENT INSPECTION OF AREA, FABRICATED REPAIR AND INSTALLED
- [SDR 7AHR201405302150](https://openairdocs.org/sdr/7AHR201405302150.md): Structure · corroded · May 30, 2014 · N742VA · Boeing 737448 · Vertical Stabilizer
  > CORROSION ON VERTICAL STABILIZER ABOVE RUDDER BALANCE WEIGHT. REMOVED CORROSION AND INSTALLED REPAIR IAW SRM 51-70-12 & 51-40-02.
- [SDR 7AHR201405202163](https://openairdocs.org/sdr/7AHR201405202163.md): Skin · corroded · May 20, 2014 · N742VA · Boeing 737448 · Wing, Plate/Skin
  > CORROSION LT WING SKIN AREA BETWEEN WS 150 & WS558. REMOVED CORROSION AND SENT MEASURMENTS TO FLIGHT VEHICLE CONSULTING FOR EVALUATION. BLENDED AREAS WERE FOUND TO BE IN LIMITS IAW FVC DWG 57-13170-1 WITH 8110-3 APPROVAL.
- [SDR 7AHR201405202311](https://openairdocs.org/sdr/7AHR201405202311.md): Spar · corroded · May 20, 2014 · N742VA · Boeing 737448 · Vertical Stabilizer, Spar/Rib
  > CORROSION FOUND ON VERTICAL STAB REAR SPAR STA 219RH SIDE REAR SPAR CHORD. REPAIR WAS ACCOMPLISHED IAW FLIGHT VEHICLE CONSULTING DWG 57-13176-1 WITH 8110-3 APPROVAL.
- [SDR 7AHR201405302368](https://openairdocs.org/sdr/7AHR201405302368.md): Window Frame · corroded · Apr 23, 2014 · N742VA · Boeing 737448 · Fuselage Main, Structure
  > EVIDENCE OF CORROSION RT SIDE PILOTS WINDOW FRAME. FLIGHT DECK CENTER WINDOW POST. R & R BY TEAM REF RELEASE VEG-RE-1302158.
- [SDR XV6A2013042700004](https://openairdocs.org/sdr/XV6A2013042700004.md): Engine · bird ingestion · Apr 27, 2013 · N742VA · Boeing 737448 · Turbine Engine Compressor Section
  > BIRD STRIKE NR 1 ENGINE, VIBRATION AT 3.8 FOR 1 MINUTE REDUCE TO BELOW 3.0 FOR THE REST OF FLIGHT. OTHER INDICATIONS NORMAL. ENGINE INSPECTED AND FOUND DAMAGE TO 8 EACH FAN BLADES. NO OTHER DEFECTS NOTED PER AMM 71-00-47 AND GMM 9-13. REMOVED AND REPLACED
- [SDR XV6A2013022700005](https://openairdocs.org/sdr/XV6A2013022700005.md): Skin · cracked · Feb 27, 2013 · N742VA · Boeing 737448 · Fuselage Main, Plate/Skin
  > DURING AN INSPECTION, FOUR CRACKS WERE FOUND IN FUSELAGE SKIN BS 727E & 727F AND BETWEEN STRINGERS 25-26L. INSTALLED REPAIR IAW SRM 53-00-00, REPAIR 31 DETAIL XXXIV.
- [SDR 2013F00073](https://openairdocs.org/sdr/2013F00073.md): Skin · cracked · Feb 27, 2013 · N742VA · Boeing 737448 · Fuselage Main, Plate/Skin
  > LT LOWER FUSELAGE SKIN BETWEEN FS 727C-727F WITH THREE NEW CRACKS ON SKIN.
- [SDR XV6A2012081200007](https://openairdocs.org/sdr/XV6A2012081200007.md): Sensor · failed · Aug 12, 2012 · N742VA · Boeing 737448 · Fuel Control/Turbine Engines
  > NR 2 ENGINE OVERTEMPED AT 938FT ON TAKEOFF FOR APPROX 1 SECOND. PERFORMED VISUAL INSPECTION OF THE INLET AND EXHAUST AREA FOR FOD AND SIGNS OF DAMAGE. NO DAMAGE OR FOD FOUND. INSPECTION WAS PERFORMED IAW B737 AMM 72-00-00 PAR. 3, SEC A, REF TO MEL 73-8 CONT
- [SDR XV6A2012070200006](https://openairdocs.org/sdr/XV6A2012070200006.md): Unknown · odor · Jul 2, 2012 · N742VA · Boeing 737448 · Air Distribution System
  > ODOR OF CHEMICALS OBSERVED IN CABIN AFTER T/O. INSPECTED BOTH LEFT AND RIGHT ACM AND THE BAY IAW B737 AMM 21-51-00. NO DEFECT FOUND. INSPECTED EQUIP COOLING SYSTEM IAW B737 AMM 21-58-51, NO DEFECT FOUND. C/W AFTER ENGINE WASH PROCEDURES IAW B737 AMM 72-00-
- [SDR XV6A2012041200002](https://openairdocs.org/sdr/XV6A2012041200002.md): Guide Vane · burned · Apr 12, 2012 · N742VA · Boeing 737448 · Fuel Injector Nozzle
  > AIR TURNBACK. NR 1 ENGINE EGT STARTED TO EXCEED 900'C ON TAKEOFF ROLL. PULLED THRUST LEVER BACK DURING CLIMB TO PREVENT EXCEEDING MAX CONTINUOUS EGT. ALSO, NR 1 ENGINE VIBE INDICATOR WAS SHOWING 4 AND 5 DURING CLIMB. PERFORMED BORESCOPE OF LPT STAGE 1 NOZZ
- [SDR ABXR2011111000051](https://openairdocs.org/sdr/ABXR2011111000051.md): Skin · corroded · Nov 10, 2011 · N742VA · Boeing 737448 · Trailing Edge Flaps
  > LOWER SKIN OF EXHAUST GATE CORRODED AT OUTBD EDGE. REMOVED FASTENERS AND REPLACED IAW B737 SRM 51-40-02 AND AMES PROCESS STANDARDS MANUAL CH 07 SECT 03 REV 09 DATED 10/6/2011.
- [SDR TIPR20090024](https://openairdocs.org/sdr/TIPR20090024.md): Floorbeam · corroded · Oct 4, 2009 · N474EA · Boeing 737448 · Fuselage Main, Floor Beam
  > FS 947.50 FLOORBEAM UPPER TEE RBL 70.53 TO LBL 70.53. REPAIRED IAW REO-G12924 REV B DATE 09/23/2009.
- [SDR TIPR20090023](https://openairdocs.org/sdr/TIPR20090023.md): Bear Strap · corroded · Oct 4, 2009 · N474EA · Boeing 737448 · Fuselage Main, Plate/Skin
  > FS 344 STR 9L TO 11L AND STR 12L TO 15L- FWD ENTRY DOOR BEARSTRAP CORRODED. REPAIRED IAW REO-G12967 REV E DATE 10/3/2009. MAJOR REPAIR.
- [SDR XV6A2009040800003](https://openairdocs.org/sdr/XV6A2009040800003.md): Battery · discharged · Apr 8, 2009 · N742VA · Boeing 737448 · Emergency Lighting
  > OVERHEAD BIN EMERGENCY LIGHTS INOP AT 18-L, 12-L, AND 10-R SEAT LOCATIONS. CHARGED EMERGENCY LIGHT SYSTEM BATTERIES IAW AMM 33-51-02.
- [SDR XV6A2009040800002](https://openairdocs.org/sdr/XV6A2009040800002.md): Battery · discharged · Apr 8, 2009 · N742VA · Boeing 737448 · Emergency Lighting
  > FLOOR LEVEL RT OVERWING EXIT IDENTIFIER LIGHT INOP. CHARGED EMERGENCY LIGHT SYSTEM BATTERIES IAW AMM 33-51-02.
- [SDR XV6A2009040600007](https://openairdocs.org/sdr/XV6A2009040600007.md): Light · inoperative · Apr 4, 2009 · N742VA · Boeing 737448 · Emergency Lighting
  > EMERGENCY LIGHTS INOP AROUND ROW 19.
- [SDR XV6A2009032000006](https://openairdocs.org/sdr/XV6A2009032000006.md): Battery Pack · discharged · Mar 19, 2009 · N742VA · Boeing 737448 · Emergency Lighting
  > LEFT OVERWING EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK IAW BOEING 737-400 AMM 33-51-51.
- [SDR XV6A2009031200004](https://openairdocs.org/sdr/XV6A2009031200004.md): Battery · discharged · Mar 11, 2009 · N742VA · Boeing 737448 · Emergency Lighting
  > R1 MAIN DOOR EMERGENCY LIGHT INOP.
- [SDR 2008FA0000538](https://openairdocs.org/sdr/2008FA0000538.md): Spar · corroded · Jul 30, 2008 · N742VA · Boeing 737448 · Trailing Edge Flaps
  > DURING SCHEDULED INSP, FOUND CORROSION ON LT IB MID FLAP, MID SPAR UPPER CHORD. (K)
- [SDR 2008FA0000514](https://openairdocs.org/sdr/2008FA0000514.md): Spar · corroded · Jul 30, 2008 · N742VA · Boeing 737448 · Trailing Edge Flaps
  > DURING SCHEDULED INSP, FOUND CORROSION ON LT IB MID FLAP, MID SPAR UPPER CHORD. (K)
- [SDR 2008FA0000513](https://openairdocs.org/sdr/2008FA0000513.md): Spar · corroded · Jul 30, 2008 · N742VA · Boeing 737448 · Trailing Edge Flaps
  > DURING SCHEDULED INSPECTION, FOUND CORROSION ON LT IB MID FLAP, MID SPAR UPPER CHORD. (K)
- [SDR 2008FA0000474](https://openairdocs.org/sdr/2008FA0000474.md): Skin · dented · Jul 9, 2008 · N742VA · Boeing 737448 · Cargo/Baggage Doors
  > DURING SCHEDULED INSPECTION, FOUND NUMEROUS DENT ON AFT CARGO EXT DOOR SKIN. S/O 312001, OPS 24422. (K)
- [SDR 2008FA0000475](https://openairdocs.org/sdr/2008FA0000475.md): Floorbeam · corroded · Jun 27, 2008 · N742VA · Boeing 737448 · Fuselage Main, Floor Beam
  > DURING SCHEDULED INSPECTION, FOUND CORROSION ON UNDERSIDE OF "T" CAP REPLACEMENT 986.5 AROUND ATTACH HOLES BL 29R TO BL 29L, NUMEROUS HOLES. (K)
- [SDR 2008FA0000393](https://openairdocs.org/sdr/2008FA0000393.md): Frame · damaged · Jun 13, 2008 · N742VA · Boeing 737448 · Fuselage Main, Frame
  > (REF DU4R2008217) DURING SCHEDULED INSPECTION, FOUND DOUBLE-DRILLED HOLE ON MAIN FRAME UPPER CAP AT BS 986.5 AT FLOOR LEVEL RT. (K)
- [SDR 2008FA0000392](https://openairdocs.org/sdr/2008FA0000392.md): Floor Support · corroded · Jun 13, 2008 · N742VA · Boeing 737448 · Fuselage Miscellaneous Structure
  > (REF DU4R2008216) DURING SCHEDULED INSPECTION, FOUND CORROSION ON UPPER SURFACE OF FLOOR SUPPORT BEAM BS 328, RBL-16 TO RBL-60. S/O NR 312001, OPS NR 24738. (K)
- [SDR 2008FA0000390](https://openairdocs.org/sdr/2008FA0000390.md): Cargo Track · corroded · Jun 10, 2008 · N742VA · Boeing 737448 · Fuselage, Seat/Cargo Attach Fittings
  > DURING SCHEDULED INSPECTION, FOUND CORROSION IN THE AFT CARGO COMPARTMENT LT TIE DOWN TRACK LBL 17.20 FROM STA 727B - STA 727E. PARTICULARLY IN FASTENER HOLE UPPER AND LOWER SURFACE. (K)
- [SDR 2008FA0000389](https://openairdocs.org/sdr/2008FA0000389.md): Skin · dented · Jun 10, 2008 · N742VA · Boeing 737448 · Fuselage Main, Plate/Skin
  > (REF DU4R2008214) DURING SCHEDULED INSPECTION, FOUND DENT ON LWR RT LOWER AFT FUSELAGE BS 887 S-19R. (K)
- [SDR 2008FA0000388](https://openairdocs.org/sdr/2008FA0000388.md): Door Frame · cracked · Jun 10, 2008 · N742VA · Boeing 737448 · Fuselage Main, Structure
  > (REF DU4R2008213) DURING SCHEDULED INSPECTION, FOUND 1 INCH LONG CRACK ON FWD CARGO DOOR CUT-OUT AFT FRAME INNER CHORD RADIUS. (K)
- [SDR 2008FA0000387](https://openairdocs.org/sdr/2008FA0000387.md): Attach Angle · corroded · Jun 10, 2008 · N742VA · Boeing 737448 · Fuselage Main, Attach Fittings
  > (REF DU4R2008212) DURING SCHEDULED INSPECTION, FOUND CORROSION IN AFT LOWER CARGO COMPARTMENT AT STA 727A ATTACH ANGLE GBGETWEEN S-27R AND S-26R. (K)
- [SDR DU4R2008211](https://openairdocs.org/sdr/DU4R2008211.md): Frame · drilled · Jun 2, 2008 · N742VA · Boeing 737448 · Fuselage Main, Frame
  > DOUBLED DRILLED HOLE IN FUSELAGE FRAME AT BS 986L.5 AT WL 208.
- [SDR DU4R2008210](https://openairdocs.org/sdr/DU4R2008210.md): Skin · dented · Jun 2, 2008 · N742VA · Boeing 737448 · Fuselage Main, Plate/Skin
  > DENT ON FUSELAGE SKIN AFT BS 910 AT S-21R.
- [SDR DU4R2008209](https://openairdocs.org/sdr/DU4R2008209.md): Skin · dented · Jun 2, 2008 · N742VA · Boeing 737448 · Fuselage Main, Plate/Skin
  > DENT ON FUSELAGE SKIN AFT BS 947 AT S-23R.
- [SDR DU4R2008208](https://openairdocs.org/sdr/DU4R2008208.md): Support · gouged · May 21, 2008 · N742VA · Boeing 737448 · Nacelle/Pylon Miscellaneous Structure
  > S/O NR312001 NR 24376, NR1 ENGINE PYLON FAN COWL SUPPORT UPPER CHORD FWD HORIZ END FLANGE NAC 166-175 APPROX IS GOUGED.
- [SDR DU4R2008207](https://openairdocs.org/sdr/DU4R2008207.md): Stringer Clip · cracked · May 18, 2008 · N742VA · Boeing 737448 · Fuselage Main, Attach Fittings
  > S/O 312001 OPS NR 24792 - CABIN BS 400 STR. 2L HAS CRACKED STRINGER CLIP.
- [SDR DU4R2008203](https://openairdocs.org/sdr/DU4R2008203.md): Floorbeam · corroded · May 11, 2008 · N742VA · Boeing 737448 · Fuselage Main, Floor Beam
  > S/O 312001 N/R 28019, CORROSION AT CABIN FLOORBEAM UPPER CHORD UPPER SURFACE BS 360 LBL 15 TO RBL 15 W/L 201.
- [SDR DU4R2008198](https://openairdocs.org/sdr/DU4R2008198.md): Frame · cracked · May 5, 2008 · N742VA · Boeing 737448 · Fuselage Main, Frame
  > S/O 312001 OPS NR 27955 - FLIGHT COMPARTMENT HAS CRACK AT SHEAR WEB FRAME BS 188 - 196 LT FLOOR LEVEL (CRACK EMANATING AT EDGE CUT OUT).
- [SDR DU4R2008197](https://openairdocs.org/sdr/DU4R2008197.md): Frame · cracked · May 5, 2008 · N742VA · Boeing 737448 · Fuselage Main, Frame
  > S/O 312001 OPS NR27954 - FLIGHT COMPARTMENT HAS CRACK AT MAIN FRAME BS 188 - 196 LT FLOOR LEVEL (CRACK AT RADIUS) OB CHORD W/L 208.
- [SDR DU4R2008196](https://openairdocs.org/sdr/DU4R2008196.md): Shear Web · cracked · May 5, 2008 · N742VA · Boeing 737448 · Fuselage Miscellaneous Structure
  > S/O 312001 OPS NR24728, FLIGHT COMPARTMENT CRACK AT SHEAR WEB BETWEEN SBS 188 - 196 RT FLOOR LEVEL (CRACK EMANATING AT EDGE CUT OUT).
- [SDR DU4R2008195](https://openairdocs.org/sdr/DU4R2008195.md): Frame · cracked · May 5, 2008 · N742VA · Boeing 737448 · Fuselage Main, Frame
  > S/O 312001 OPS NR 24727 - CRACK AT MAIN FRAME OB CHORD STA. 188 RT SIDE FLOOR LEVEL (CRACK IN RADIUS).
- [SDR DU4R2008193](https://openairdocs.org/sdr/DU4R2008193.md): Skin · dented · May 5, 2008 · N742VA · Boeing 737448 · Fuselage Main, Plate/Skin
  > S/O 312001 OPS NR 24422 - AFT CARGO EXT DOOR SKIN HAS OUT OF LIMIT DENTS BETWEEN 2 EA EXISTING REPAIRS.
- [SDR DU4R2008194](https://openairdocs.org/sdr/DU4R2008194.md): Structure · corroded · May 5, 2008 · N742VA · Boeing 737448 · Passenger/Crew Doors
  > S/O 312001 OPS NR 24701, CORROSION OUT OF LIMITS ON L-1 DOOR LOWER INNER CHORD AT BS 328, LBL 58 TO LBL 60.
- [SDR DU4R2008201](https://openairdocs.org/sdr/DU4R2008201.md): Floorbeam · corroded · May 2, 2008 · N742VA · Boeing 737448 · Fuselage Main, Floor Beam
  > S/O 312001 N/R 24738 - CORROSION ON UPPER SURFACE OF FLOOR SUPPORT BEAM BS 328 RBL 16 - RBL 60.
- [SDR DU4R2008200](https://openairdocs.org/sdr/DU4R2008200.md): Floorbeam · corroded · May 2, 2008 · N742VA · Boeing 737448 · Fuselage Main, Floor Beam
  > S/O 312001 N/R 24703 - CORROSION ON TOP OF FLOORBOARD IN GOUGE BS 312 LBL 52 TO LBL 8, AND NUMEROUS PLACES AT RBL 0 TO RBL-54.

Next page: https://openairdocs.org/model/boeing-737-448/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 = '737448'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-737-448/reports

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