# Service difficulty reports: N383US, cancelled Jul 25, 2006

A list on [N383US, cancelled Jul 25, 2006](https://openairdocs.org/deregistered/N383US-2006-07-25.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 4 · 151 reports

- [SDR SB05119](https://openairdocs.org/sdr/SB05119.md): Adc · failed · Sep 23, 2005 · N383US · Boeing 7373B7 · Air Data Computer
  > CLT FLT448 ON TAKEOFF ROLL, WITH FIRST OFFICER FLYING, THE FIRST OFFICER LOST AIRSPEED INDICATOR, ALTIMETER AND VERTICAL SPEED. AFTER TRANSFER OF CONTROLS TO CAPTAIN, THE FLIGHT RETURNED TO FIELD AT CLT. FLIGHT LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DE
- [SDR USAA050464](https://openairdocs.org/sdr/USAA050464.md): Skin · cracked · Apr 2, 2005 · N383US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > PIT - FOUND SKIN CRACKED 1.5 INCH LONG, BS 747 BETWEEN 19L AND 20L. INSTALLED DOUBLER SKIN REPAIR PER EA 83173, SRM 53-00-01. (M)
- [SDR SB05036](https://openairdocs.org/sdr/SB05036.md): Pressure Switch · faulty · Mar 3, 2005 · N383US · Boeing 7373B7 · APU Oil System
  > BWI - FLT141 - EN ROUTE FROM DCA TO IND, AT FL270, WITH THE APU POWERING THE NR 2 GENERATOR BUS, THE APU LOW OIL PRESSURE LIGHT ILLUMINATED FOLLOWED BY AN APU AUTO SHUT DOWN. THE NR 2 ENGINE CSD WAS ALREADY ON MEL SO THE FLIGHT DIVERTED TO BWI AND LANDED WITH
- [SDR SB05027](https://openairdocs.org/sdr/SB05027.md): Battery Pack · discharged · Feb 18, 2005 · N383US · Boeing 7373B7 · Emergency Lighting
  > PHL - MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHTS ABOVE THE AFT LEFT SERVICE DOOR AND THE AFT RIGHT SERVICE DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACKS. OPERATIONAL CHECK GOOD.
- [SDR SB04169](https://openairdocs.org/sdr/SB04169.md): Logic Card · dirty · Dec 21, 2004 · N383US · Boeing 7373B7 · Landing Gear Position and Warning
  > ALB - FLT1231 - ON APPROACH TO ALB FROM CLT, THE RIGHT MAIN LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE WHEN GEAR WAS EXTENDED. CREW PERFORMED MANUAL GEAR EXTENSION PROCEDURE AND RECEIVED ALL THREE GREEN GEAR LIGHTS. CREW REPORTED LIGHTS TESTED OK. FLIGHT L
- [SDR USAA040866](https://openairdocs.org/sdr/USAA040866.md): Skin · cracked · Nov 11, 2004 · N383US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > SKIN, 1.75 INCHES CRACKED AT STA 927 AND 947.5 AT STR 25R. INSTALLED DOUBLER REPAIR IAW SRM 53-00-01.
- [SDR USAA040786](https://openairdocs.org/sdr/USAA040786.md): Floor Support · corroded · Oct 29, 2004 · N383US · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > PIT - Q5, FLOOR SUPPORT,.1250 INCH BY.1250 INCH AREA, CORROSION; LEVEL 1; TASK NRC53-107-02, FASTENER HOLE AT STA 947 RBL 20. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR ANGLE, SHIM AND FILLER IAW EA 79192.
- [SDR USAA040798](https://openairdocs.org/sdr/USAA040798.md): Channel · cracked · Oct 29, 2004 · N383US · Boeing 7373B7 · Nacelle/Pylon Miscellaneous Structure
  > PIT, Q5, CHANNEL, 6 INCH LONG CRACK, NR 2 PYLON LOWER CHANNEL NAC STA 363. REMOVED AND REPLACED CHANNEL IAW SRM 51-10-02.
- [SDR USAA040782](https://openairdocs.org/sdr/USAA040782.md): Skin Panel · damaged · Oct 23, 2004 · N383US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > PIT, Q5, SKIN PANEL, REMOVED AND REPLACED SKIN PANEL AT BS 980 FROM S20R-S25R. REMOVED AND REPLACED SKIN PANEL DUE TO TEMPORARY REPAIRS; REPAIR TOO CLOSE TO LAP JOINTS; IAW EO 79060.
- [SDR USAA040793](https://openairdocs.org/sdr/USAA040793.md): Threshold · corroded · Oct 23, 2004 · N383US · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > PIT,Q5, THRESHOLD, 2 INCH X 4 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-202-01 AFT CARGO DOOR THRESHOLD S25R. INSTALLED THRESHOLD IAW DWG 65-47957. AFT CARGO DOOR THRESHOLD S25R.
- [SDR USAA040795](https://openairdocs.org/sdr/USAA040795.md): Frame · corroded · Oct 23, 2004 · N383US · Boeing 7373B7 · Fuselage Main, Frame
  > PIT, Q5, FRAME.2500 INCH X.2500 INCH- 6 EA AREAS, CORROSION; LEVEL 1; TASK NR C53-208-01 AROUND FASTENER HOLES - STA 847 FRAME BETWEEN S26R, ES25R. SPLICED IN NEW FRAME SECTION IAW EA 79270.
- [SDR USAA040794](https://openairdocs.org/sdr/USAA040794.md): Intercostal · corroded · Oct 19, 2004 · N383US · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > PIT, Q5, INTERCOSTAL,.5000 INCH AND.2500 INCH, 2 BRACKETS, CORROSION; NO LEVEL OR TASK. E11 DOOR FRAME AT SWITCH NR 3196 INSIDE OF FRAME, BL0, STA 203.8. FABRICATED ANGLES, REPLACED IAW SRM 53-00-04.
- [SDR USAA040827](https://openairdocs.org/sdr/USAA040827.md): Pressure Blkhd · damaged · Oct 18, 2004 · N383US · Boeing 7373B7 · Fuselage Main, Bulkhead
  > PIT - Q5, AFT PRESSURE BULKHEAD, NUMEROUS TENSION BOLTS LOOSE, STA 1016 AFT PRESSURE BULKHEAD. REPLACED TENSION BOLTS IAW EA 79074 AND SB 737-53-1229.
- [SDR USAA040828](https://openairdocs.org/sdr/USAA040828.md): Tee Fitting · defective · Oct 13, 2004 · N383US · Boeing 7373B7 · Fuselage Main, Bulkhead
  > STRINGER T FITTING, NO EDGE DISTANCE. NO EDGE DISTANCE FOR FASTENERS, FWD SIDE AFT PRESSURE BULKHEAD AT S10L. DEFECTIVE PART REPLACED WITH IDENT PART IAW MFG DWG 65-49914, DASH NR 535, EA 79074.
- [SDR USAA040825](https://openairdocs.org/sdr/USAA040825.md): Frame · cracked · Oct 8, 2004 · N383US · Boeing 7373B7 · Fuselage Main, Frame
  > PIT - Q5, FRAME, CRACKED, (2EA) 2 INCHES AND 2.2500 INCH, 727D BETWEEN S-27L AND S-27R AT 1 RBBL AND LBBL. REPAIRED DOUBLER IAW SRM 51-70-11.
- [SDR USAA040826](https://openairdocs.org/sdr/USAA040826.md): Attach Fitting · chafed · Oct 2, 2004 · N383US · Boeing 7373B7 · Vertical Stabilizer, Attach Fittings
  > PIT - Q5, FITTINGS,.1250,.5,.5,.5 INCH AREAS, HEAVY CHAFING (4 AREAS), ALL 4 AFT LUGS OF VERT STAB ATTACH FITTINGS.
- [SDR USAA040785](https://openairdocs.org/sdr/USAA040785.md): Seat Track · corroded · Oct 2, 2004 · N383US · Boeing 7373B7 · Fuselage, Seat/Cargo Attach Fittings
  > PIT - Q5, SEAT TRACK, 2 INCH BY 4 INCH CORRODED AREA, LEVEL 1 TASK NR C53-107-02, AFT END OF RT OB SEAT TRACK, STA 947. MANUFACTURED FILLERS AND SPLICED IN A NEW SECTION IAW SRM 53-00-52.
- [SDR USAA040789](https://openairdocs.org/sdr/USAA040789.md): Floorbeam · corroded · Oct 2, 2004 · N383US · Boeing 7373B7 · Fuselage Main, Floor Beam
  > PIT - Q5, FLOORBEAM TEE CAP,.1250 INCH BY.1250 INCH (6 AREAS), CORROSION; LEVEL 1; TASK NR C53-107-02, TOPS OF FLOORBEAMS IN AROUND SCREW HOLES STA 1016-986.5. REMOVED CORROSION, TREATED, PRIMED, REPLACED 10 INCHES OF T-CAP IAW SRM 53-60-51.
- [SDR USAA040790](https://openairdocs.org/sdr/USAA040790.md): Channel · corroded · Oct 2, 2004 · N383US · Boeing 7373B7 · Service Doors
  > PIT,Q5, Z-CHANNEL, 4 INCH X 1 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-107-01, FWD SERVICE DOOR Z-CHANNEL. REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR USAA040799](https://openairdocs.org/sdr/USAA040799.md): Floorbeam · cracked · Oct 2, 2004 · N383US · Boeing 7373B7 · Fuselage Main, Floor Beam
  > PIT, Q5, FLOORBEAM, 3 INCH CRACK (BROKEN).400 INCH CRACK, STA 540 LBL 1 AND LBL 19 SUPPORT). REMOVED AND REPLACED WITH NEW FLOOR SUPPORT IAW SRM 53-21-00.
- [SDR USAA040800](https://openairdocs.org/sdr/USAA040800.md): Bracket · cracked · Oct 2, 2004 · N383US · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > PIT, Q5, BRACKET, 1 INCH X.2500 INCH CRACK, (L) BRACKET, STA 350 RBL 20. FABRICATED NEW BRACKET IAW DWG 69-74588.
- [SDR USAA040801](https://openairdocs.org/sdr/USAA040801.md): Floor Support · cracked · Oct 2, 2004 · N383US · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > PIT, Q5, FLOOR SUPPORT WITH.2500 INCH X.3750 INCH CRACKS, END OF FLOOR SUPPORT, STA 540 LT AND RT OF BL-0. REMOVED AND REPLACED IAW SRM 53-21-00.
- [SDR USAA040784](https://openairdocs.org/sdr/USAA040784.md): Skin · cracked · Oct 1, 2004 · N383US · Boeing 7373B7 · Leading Edge Devices
  > PIT - Q5, NR 1 SLAT,.2500 INCH CRACK, NR 1 SLAT L/E LOWER SURFACE AFT ROW OF RIVETS. DOUBLER INSTALLED IAW 57-43-01.
- [SDR USAA040791](https://openairdocs.org/sdr/USAA040791.md): Floor Support · corroded · Sep 30, 2004 · N383US · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > PIT, Q5, ANGLE/TRACK, 2 INCH CORROSION, LEVEL 1; TASK NR C53-202-01 AFT CARGO CORE, FLOOR TIE DOWN TRACK, STA 859 LBL 17.20. SPLICED REPAIR SECTION INTO FLOOR TRACK IAW SRM 53-00-53.
- [SDR USAA040821](https://openairdocs.org/sdr/USAA040821.md): Channel · cracked · Sep 30, 2004 · N383US · Boeing 7373B7 · Nacelle/Pylon Miscellaneous Structure
  > PIT, Q5, CHANNEL WITH A 4 INCH LONG CRACK IN LOWER CHANNEL AT NR 2 NAC, STA 345. REMOVED AND REPLACED CHANNEL IAW SRM 51-10-02.
- [SDR USAA040788](https://openairdocs.org/sdr/USAA040788.md): Keelbeam · corroded · Sep 25, 2004 · N383US · Boeing 7373B7 · Fuselage Main, Structure
  > PIT Q5, KEEL BEAM, 2 INCHES X 40 INCHES AREA CORROSION; LEVEL 1 TASK NR C53-208-01, L KEEL BEAM STA 500D-540. REMOVED AND REPLACED, SPLICED IN NEW SECTION IAW TYP REP 53-60-09.
- [SDR USAA040802](https://openairdocs.org/sdr/USAA040802.md): Skin · cracked · Sep 21, 2004 · N383US · Boeing 7373B7 · Nacelle/Pylon, Plate/Skin
  > PIT, Q5, SKIN, 6 INCH CRACK, RT PYLON LOWER PAN FROM NAC 319 AFT TO END. REMOVED AND REPLACED SKIN AND INSTALLED DOUBLER IAW SRM 51-70-13.
- [SDR USAA040781](https://openairdocs.org/sdr/USAA040781.md): Intercostal · damaged · Sep 16, 2004 · N383US · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > PIT, Q5, INTERCOSTAL, HOLE DAMAGE. LIGHTENING HOLE DAMAGE, STA 294.5 + 312 LBL 10 INCH INTERCOSTAL FLOORBEAM LIGHTENING HOLE DAMAGE. FABRICATED WEB AND INSTALLED SAME IAW 53-10-51, FIG 1, PG 17.
- [SDR USAA040792](https://openairdocs.org/sdr/USAA040792.md): Angle · corroded · Sep 14, 2004 · N383US · Boeing 7373B7 · Fuselage Main, Keel
  > PIT, Q5, KEEP REPAIR ANGLE, 20 INCH AREA, CORROSION; LEVEL 1; TASK NR C 53-208-01 R KEEL STA 520-540. INSTALLED NEW REPAIR ANGLE/ DOUBLER IAW SRM 51-70-11.
- [SDR USAA040805](https://openairdocs.org/sdr/USAA040805.md): Door Frame · cracked · Sep 13, 2004 · N383US · Boeing 7373B7 · Fuselage Main, Structure
  > PIT, Q5, WEB FRAME, 3 INCH CRACK AT FWD ENTRY DOOR LOWER WEB FRAME FORWARD CORNER. FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 52-10-02 FIG 1, SRM 51-70-11 FIG 1.
- [SDR USAA040787](https://openairdocs.org/sdr/USAA040787.md): Floor Support · corroded · Sep 12, 2004 · N383US · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > PIT, Q5, FLOOR SUPPORT, 4 INCH X 3 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-107-02 FLOOR SUPPORT, STA 986.5 RT BL0. DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM 53-60-51.
- [SDR USAA040797](https://openairdocs.org/sdr/USAA040797.md): Angle · corroded · Sep 12, 2004 · N383US · Boeing 7373B7 · Passenger/Crew Doors
  > PIT, Q5, Z-ANGLE, 4 INCHES LONG, CORROSION; LEVEL 1 TASK NR C53-107-01 AFT ENT DOOR Z-ANGLE. DEFECTIVE PART REPLACED WITH IDENT PART IAW MFG DWG.
- [SDR USAA040824](https://openairdocs.org/sdr/USAA040824.md): Keelbeam · cracked · Sep 11, 2004 · N383US · Boeing 7373B7 · Fuselage Main, Keel
  > PIT - Q5, KEEL REPAIR ANGLE,.2500 INCH CRACK, FASTENER HOLE, STA 520 ON KEELBEAM REPAIR ANGLE RT. REPAIR ANGLES/DOUBLER INSTALLED IAW SRM 51-70-11.
- [SDR USAA040803](https://openairdocs.org/sdr/USAA040803.md): Skin · delaminated · Sep 10, 2004 · N383US · Boeing 7373B7 · Leading Edge Devices
  > PIT, Q5, TOP SKIN AND CORE BOND, 3.5 INCH AREA. DELAMINATION, NR 4 SLAT OB END TOP SURFACE. REMOVED DAMAGE, INSTALLED NEW CORE SECTION AND DOUBLER IAW SRM 51-70-10.
- [SDR USAA040804](https://openairdocs.org/sdr/USAA040804.md): Skin · delaminated · Sep 10, 2004 · N383US · Boeing 7373B7 · Spoilers
  > PIT, Q5, TOP SKIN - CORE BOND 1 INCH AREA, DELAMINATION, LT WING NR 1 SPOILER AT AFT OB CORNER - TOP SURFACE. REMOVED DAMAGED AREA, INSTALLED FILLER AND DOUBLER IAW SRM 51-70-10.
- [SDR USAA040808](https://openairdocs.org/sdr/USAA040808.md): Skin · delaminated · Sep 10, 2004 · N383US · Boeing 7373B7 · Leading Edge Devices
  > PIT, O5, TOP SKIN- CORE BOND, 2 INCH AREA. NR 4 SLAT IB END TOP SURFACE. REMOVED DAMAGED SKIN AND CORE, INSTALLED NEW CORE AND DOUBLER IAW SRM 51-70-10.
- [SDR USAA040807](https://openairdocs.org/sdr/USAA040807.md): Spar · cracked · Sep 9, 2004 · N383US · Boeing 7373B7 · Vertical Stabilizer, Spar/Rib
  > PIT, Q5, ANGLE SUPPORT.7500 INCH CRACK, VERT STAB SPAR ANGLE FOR RIB 163.90 FRONT LT SIDE. INSTALLED DOUBLER AND SHIM IAW EA 79100.
- [SDR USAA040806](https://openairdocs.org/sdr/USAA040806.md): Skin · debonded · Sep 8, 2004 · N383US · Boeing 7373B7 · Trailing Edge Flaps
  > PIT, Q5, TOP SKIN - CORE BOND, 3 INCH X 3 INCH AREA, DEBONDED. LT IB AFT FLAP, UPPER OB T/E. REMOVED DAMAGE, INSTALLED CORE, DOUBLER IAW TR 57-53-01A, EA 79082, SRM 51-70-10.
- [SDR USAA040796](https://openairdocs.org/sdr/USAA040796.md): Floor Support · corroded · Sep 5, 2004 · N383US · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > PIT, Q5, FLOOR SUPPORT 1 INCH 10 INCH AREA. CORROSION; LEVEL 1; TASK NR C53-107-02 LOCATED AT STA 986.5 TO 1016, RBL 3.54 TO RBL 18.25. DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM 51-10-02.
- [SDR USAA040809](https://openairdocs.org/sdr/USAA040809.md): Skin · delaminated · Sep 3, 2004 · N383US · Boeing 7373B7 · Leading Edge Devices
  > PIT, Q5, TOP SKIN - CORE BOND, 2 INCH AREA AT NR 5 SLAT T/E; 1 AT IB END AND 1 AT OB END. REMOVED DELAMINATED AREA, INSTALLED NEW TOP SKIN IAW SRM 51-70-10.
- [SDR USAA040815](https://openairdocs.org/sdr/USAA040815.md): Clip · cracked · Sep 1, 2004 · N383US · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > PIT, Q5, CLIP 1 INCH CRACK, STR 19 AND STA 986 BULKHEAD. INSTALLED CLIP IAW SRM 5-40-02.
- [SDR USAA040820](https://openairdocs.org/sdr/USAA040820.md): Crease Beam · cracked · Sep 1, 2004 · N383US · Boeing 7373B7 · Fuselage Main, Structure
  > PIT, Q5, CREASE BEAM WEB 1 INCH CRACK. LT CREASE BEAM BS 616-639. DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM 51-10-02.
- [SDR USAA050822](https://openairdocs.org/sdr/USAA050822.md): Skin · worn · Sep 1, 2004 · N383US · Boeing 7373B7 · Trailing Edge Flaps
  > MID FLAP L/E, 24 INCHES WORN. IB 24 INCHES ON THE LT OB MID FLAP L/E AT IB END. INSTALLED DOUBLER IAW SRM 57-53-01, FIG 208.
- [SDR USAA040783](https://openairdocs.org/sdr/USAA040783.md): Stringer Clip · cracked · Aug 29, 2004 · N383US · Boeing 7373B7 · Fuselage Main, Attach Fittings
  > PIT - Q5, TIE-.1250 INCH CRACK, RIVET, STR TO FRAME CLIP, STA 663.75-S10R. REMOVED AND REPLACED STRINGER CLIP (TIE) IAW 53-00-03.
- [SDR USAA040812](https://openairdocs.org/sdr/USAA040812.md): Clip · cracked · Aug 29, 2004 · N383US · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > PIT, Q5, CLIP EST..125 INCH STA 500D S 8L. REPLACED CLIP IAW SRM 51-10-02 AND 51-40.
- [SDR USAA040813](https://openairdocs.org/sdr/USAA040813.md): Clip · cracked · Aug 29, 2004 · N383US · Boeing 7373B7 · Fuselage Main, Structure
  > PIT, Q5, CLIP EST..125 INCH CRACK, STA 500B S 10L. REPLACED CLIP IAW SRM 51-10-02 AND 51-40.
- [SDR USAA040814](https://openairdocs.org/sdr/USAA040814.md): Clip · cracked · Aug 29, 2004 · N383US · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > PIT, Q5, CLIP EST..125 INCH CRACK, STA 440S 10L. REPLACED CLIP IAW SRM 51-10-02 AND 51-40.
- [SDR USAA040823](https://openairdocs.org/sdr/USAA040823.md): Clip · cracked · Aug 29, 2004 · N383US · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > CLIP, EST..125 INCH CRACK, STA 500D SGL. REMOVED AND REPLACED CLIP IAW SRM 51-10-02, 51-40.
- [SDR USAA040810](https://openairdocs.org/sdr/USAA040810.md): Stringer Clip · cracked · Aug 28, 2004 · N383US · Boeing 7373B7 · Fuselage Main, Attach Fittings
  > PIT, Q5, STRINGER CLIPS,.5000 INCH AND.1250 INCH CRACKS, STA 578, STR S9R. CLIP REPLACED IAW SRM 51-40-02.
- [SDR USAA040819](https://openairdocs.org/sdr/USAA040819.md): Skin · cracked · Aug 28, 2004 · N383US · Boeing 7373B7 · Leading Edge Devices
  > PIT, Q5, SKIN WITH 1.2500 INCH CRACKS (3 EA). NR 1 SLAT, LOWER SURFACE AT ROW IB END 4TH RIVET. INSTALLED DOUBLER IAW SRM 57-43-01, FIG 206.

Next page: https://openairdocs.org/deregistered/N383US-2006-07-25/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 n_number = 'N383US' AND deregistration_id = 'N383US-2006-07-25'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N383US-2006-07-25/reports

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