# Service difficulty reports: N740AS

A list on [N740AS](https://openairdocs.org/aircraft/N740AS.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 7 · 350 reports

- [SDR ASAA0611123](https://openairdocs.org/sdr/ASAA0611123.md): Battery · discharged · Oct 21, 2006 · N740AS · Boeing 737290C · Emergency Lighting
  > SMOKE BARRIER NR 8 EXIT TO REAR LIGHT DIM. REPLACED EMERGENCY EXIT LIGHT BATTERY.
- [SDR ASAA0611033](https://openairdocs.org/sdr/ASAA0611033.md): Battery Pack · discharged · Sep 27, 2006 · N740AS · Boeing 737290C · Emergency Lighting
  > SMOKE BARRIER NR 8 EMERGENCY EXIT LIGHT WILL NOT ILLUMINATE. REPLACED BATTERY PACK, OPS OKAY.
- [SDR ASAA0610961](https://openairdocs.org/sdr/ASAA0610961.md): Battery Pack · discharged · Sep 12, 2006 · N740AS · Boeing 737290C · Emergency Lighting
  > BULKHEAD EMERGENCY EXIT LIGHT CAME ON DURING FLIGHT. REPLACED SMOKE BARRIER -EXIT TO REAR- EMERGENCY EXIT SIGN BATTERY PACK.
- [SDR ASAA0610647](https://openairdocs.org/sdr/ASAA0610647.md): Battery · discharged · May 25, 2006 · N740AS · Boeing 737290C · Emergency Lighting
  > FOUND EMERGENCY EXIT LIGHT OVER L1 DOOR INOP, INSTALLED NEW BATTERY.
- [SDR ASAA0610521](https://openairdocs.org/sdr/ASAA0610521.md): Skin · cracked · May 1, 2006 · N740AS · Boeing 737290C · Fuselage Main, Plate/Skin
  > FOUND 2.5 INCH CRACK ON THE RIGHT SIDE OF FUSELAGE. REPAIRED PER SRM 53 30 3.
- [SDR ASAA0610273](https://openairdocs.org/sdr/ASAA0610273.md): Battery Pack · discharged · Mar 24, 2006 · N740AS · Boeing 737290C · Emergency Lighting
  > R2 DOOR EMERGENCY LIGHT ABOVE DOOR WILL NOT SHUT OFF. REPLACED BATTERY PACK.
- [SDR ASAA0610226](https://openairdocs.org/sdr/ASAA0610226.md): Check Valve · sticking · Mar 3, 2006 · N740AS · Boeing 737290C · Landing Gear Retraction/Extension System
  > NLG UNSAFE LIGHT AND A SYSTEM LOW PRESSURE. REMOVED AND REPLACED FILTER AND MANIFOILD AND AIR PRESS REG CHECK VLV. JACKED AND RETRACTED NLG, OPS CHK GOOD, SYS OPS CHK NML.
- [SDR ASAA0610109](https://openairdocs.org/sdr/ASAA0610109.md): Battery · discharged · Feb 2, 2006 · N740AS · Boeing 737290C · Emergency Lighting
  > LT EMERGENCY LIGHT UNDER DOOR IS INOP. CHANGED BATTERY OPS CHK GOOD.
- [SDR ASAA0510335](https://openairdocs.org/sdr/ASAA0510335.md): Skin · bulged · Sep 30, 2005 · N740AS · Boeing 737290C · Fuselage Main, Plate/Skin
  > YXX - FOUND FUSELAGE SKIN BULGING AT BS 535 AT RT KEEL BEAM. SKIN AT BS 535 AND RT KEEL BEAM WAS REPAIRD IAW ASA EA5360-01040. (M)
- [SDR ASAA0510334](https://openairdocs.org/sdr/ASAA0510334.md): Floorbeam · corroded · Sep 29, 2005 · N740AS · Boeing 737290C · Fuselage Main, Floor Beam
  > YXX - UPPER CHORD OF BS 344 FLOORBEAM CORRODED FROM RBL 5-10, UNDER FASTENER HEADS AND ON SURFACE. REPLACED WITH REPAIR PARTS IAW B737-200 SRM 53-10-9. (M)
- [SDR ASAA0510333](https://openairdocs.org/sdr/ASAA0510333.md): Floorbeam · corroded · Sep 29, 2005 · N740AS · Boeing 737290C · Fuselage Main, Floor Beam
  > YXX - FOUND EXFOLIATING CORROSION FOUND ON UPPER CHORD OF FLOORBEAM. REPLACED WITH REPAIR PARTS IAW B737-200 SRM 53-10-9. (M)
- [SDR ASAA0510332](https://openairdocs.org/sdr/ASAA0510332.md): Splice · corroded · Sep 29, 2005 · N740AS · Boeing 737290C · Fuselage Miscellaneous Structure
  > YXX - FOUND CORROSION ON STRINGER SPLICE AT BS 357-369 STRINGER 28 LEFT. REPAIRED STRINGER SPLICE AT BS 357-369, STRINGER 29 LEFT IAW B737-200 SRM 51-40-3. (M)
- [SDR ASAA0510331](https://openairdocs.org/sdr/ASAA0510331.md): Stringer Clip · cracked · Sep 29, 2005 · N740AS · Boeing 737290C · Fuselage Main, Attach Fittings
  > YXX - FOUND TIE CLIP CRACKED AT STRINGER 2 RT BS 639. REPLACED IAW B737-200 SRM 51-30-02 FIGURE 3. (M)
- [SDR ASAA0510330](https://openairdocs.org/sdr/ASAA0510330.md): Shear Tie · corroded · Sep 29, 2005 · N740AS · Boeing 737290C · Fuselage Internal Mounting Structure
  > YXX - FOUND CORROSION ON SKIN TO FRAME AT BS 360 BETWEEN STRINGER 25 RT AND 26 RT. REPLACED IAW B737-200 SRM 53-10-4 FIGURE 8. (M)
- [SDR ASAA0510329](https://openairdocs.org/sdr/ASAA0510329.md): Doubler · dented · Sep 29, 2005 · N740AS · Boeing 737290C · Fuselage Main, Frame
  > YXX - FOUND FRAME DOUBLER DAMAGED AT BS 360 BETWEEN STRINGER 26 RT PLUS 4 INCHES TO STRINGER 28 RT. REPLACED DOUBLER IAW B737-200 SRM 51-40-3. (M)
- [SDR ASAA0510328](https://openairdocs.org/sdr/ASAA0510328.md): Skin · gouged · Sep 29, 2005 · N740AS · Boeing 737290C · Fuselage Main, Plate/Skin
  > YXX - FOUND GOUGE IN AIRCRAFT SKIN 2 INCHES ABOVE STRINGER 22 LEFT AT BS 1010. REPAIRED IAW B737-200 SRM 51-10-1 FIGURE 1, 51-30-05 FIGURE 4 AND 51-30-02 FIGURE 4. (M)
- [SDR ASAA0510327](https://openairdocs.org/sdr/ASAA0510327.md): Frame · cracked · Sep 29, 2005 · N740AS · Boeing 737290C · Fuselage Main, Frame
  > YXX - FOUND FORWARD CARGO PIT FRAME CRACKED AT BS 460 BETWEEN STRINGER 22 AND 23 LEFT. REPLACED FRAME WITH REPAIR PARTS PER B737-200 SRM 53-10-4. (M)
- [SDR ASAA0510323](https://openairdocs.org/sdr/ASAA0510323.md): Clevis · corroded · Sep 22, 2005 · N740AS · Boeing 737290C · Vertical Stabilizer, Spar/Rib
  > YXX - FOUND CORROSION ON VERTICAL STABILIZER AFT SPAR LEFT PRIMARY FORWARD CLEVIS FORWARD FACE. FACES MACHINED PER EA 5340-01138. (M)
- [SDR ASAA0510322](https://openairdocs.org/sdr/ASAA0510322.md): Clevis · corroded · Sep 22, 2005 · N740AS · Boeing 737290C · Vertical Stabilizer, Spar/Rib
  > YXX - FOUND CORROSION ON VERTICAL STABILIZER AFT SPAR RIGHT PRIMARY FORWARD CLEVIS FORWARD FACE. CLEVIS REPLACED PER BOEING DWG 6546575 AND B737-200 SRM 51-30-2 PARAGRAPH 17. (M)
- [SDR ASAA0510321](https://openairdocs.org/sdr/ASAA0510321.md): Clevis · corroded · Sep 22, 2005 · N740AS · Boeing 737290C · Vertical Stabilizer, Spar/Rib
  > YXX - FOUND CORROSION ON VERTICAL STABILIZER AFT SPAR RIGHT PRIMARY FORWARD CLEVIS AFT FACE. CLEVIS REPLACED PER BOEING DWG 6546575 AND B737-200 SRM 51-30-2 PARAGRAPH 17. (M)
- [SDR ASAA0510320](https://openairdocs.org/sdr/ASAA0510320.md): Spar · corroded · Sep 22, 2005 · N740AS · Boeing 737290C · Vertical Stabilizer, Spar/Rib
  > YXX - FOUND CORROSION ON VERTICAL STABILIZER AFT SPAR RIGHT PRIMARY AFT CLEVIS FORWARD FACE. CLEVIS REPLACED PER BOEING DWG 65-46572 AND B737-200 SRM 51-30-2. (M)
- [SDR ASAA0510319](https://openairdocs.org/sdr/ASAA0510319.md): Clevis · corroded · Sep 22, 2005 · N740AS · Boeing 737290C · Vertical Stabilizer, Spar/Rib
  > YXX - FOUND CORROSION ON VERTICAL STABILIZER AFT SPAR RIGHT PRIMARY AFT CLEVIS AFT FACE. CLEVIS REPLACED PER EA 5340-01137. (M)
- [SDR ASAA0510324](https://openairdocs.org/sdr/ASAA0510324.md): Clevis · corroded · Sep 22, 2005 · N740AS · Boeing 737290C · Elevator, Spar/Rib
  > CORROSION ON VERTICAL STABILIZER AFT SPAR LT FAIL SAFE CLEVIS FACES NOT PARALLEL TO EACH OTHER. FACES MACHINED IAW EA. (K)
- [SDR ASAA0510318](https://openairdocs.org/sdr/ASAA0510318.md): Floorbeam · corroded · Sep 21, 2005 · N740AS · Boeing 737290C · Fuselage Main, Floor Beam
  > FOUND EXFOLIATION CORROSION FOUND ON UPPER CHORD OF FLOORBEAM AT BS 328, FROM BL 0 -RBL 56. CHORD REPLACED IAW SRM 53-10-9.
- [SDR ASAA0510317](https://openairdocs.org/sdr/ASAA0510317.md): Stringer Splice · corroded · Sep 21, 2005 · N740AS · Boeing 737290C · Fuselage Miscellaneous Structure
  > YXX - FOUND CORROSION ON STRINGER SPLICE AT BS 370-380 STRINGER 27 RT. STRINGER SPLICE REPLACED PER B737-200 SRM 51-30-2. (M)
- [SDR ASAA0510316](https://openairdocs.org/sdr/ASAA0510316.md): Floor Support · corroded · Sep 21, 2005 · N740AS · Boeing 737290C · Fuselage Miscellaneous Structure
  > YXX - FOUND CORROSION AT 5 CLIP NUT LOCATIONS ON FLOOR SUPPORT STRUCTURE LOCATED AT LBL 40, WL 207, BS 312-344. FLOOR SUPPORT CHORD REPAIRED BY REPLACEMENT PER B737-200 SRM 51-30-2. (M)
- [SDR ASAA0510315](https://openairdocs.org/sdr/ASAA0510315.md): Skin · corroded · Sep 21, 2005 · N740AS · Boeing 737290C · Fuselage Main, Plate/Skin
  > YXX - FOUND IN FORWARD CARGO BAY CORROSION ON SKIN AT BS 360-380 AT STRINGER 27 RT. SKIN REPAIRED PER B737-200 SRM 53-30-3. (M)
- [SDR ASAA0510314](https://openairdocs.org/sdr/ASAA0510314.md): Floorbeam · corroded · Sep 20, 2005 · N740AS · Boeing 737290C · Fuselage Main, Floor Beam
  > YXX - FOUND UPPER CHORD OF BS 344 FLOORBEAM CORRODED FROM RBL 5-10, UNDER FASTENER HEADS AND ON SURFACE. REMOVED AND REPLACED UPPER CHORD PER B737-200 SRM 53-10-9. (M)
- [SDR ASAA0510313](https://openairdocs.org/sdr/ASAA0510313.md): Floorboard · corroded · Sep 20, 2005 · N740AS · Boeing 737290C · Fuselage Floor Panel
  > YXX - IN FORWARD CARGO PIT CORROSION ON LOWER CHORD OF CABIN FLOOR BOARD AT BS 420 LBL 36-44 BETWEEN PREVIOUS REPAIR PARTS. THE LOWER CHORD OF CABIN FLOORBEAM AT BS 420 FROM LBL 36-44 WAS REPAIRED IAW EA 5310-02491. (M)
- [SDR ASAA0510312](https://openairdocs.org/sdr/ASAA0510312.md): Stringer Splice · damaged · Sep 20, 2005 · N740AS · Boeing 737290C · Fuselage Miscellaneous Structure
  > YXX - FOUND STRINGER SPLICE AT BS 365-350 AT STRINGER 26 RT HAS ELONGATED HOLES. REPLACED STRINGER SPLICE IAW B737-200 SRM 51-30-5 FIGURE 3. (M)
- [SDR ASAA0510311](https://openairdocs.org/sdr/ASAA0510311.md): Stringer Splice · damaged · Sep 20, 2005 · N740AS · Boeing 737290C · Fuselage Miscellaneous Structure
  > YXX - FOUND STRINGER SPLICE AT BS 365 TO 350 AT STRINGER 27 LEFT HAS ELONGATED HOLES. REPLACED STRINGER SPLICE IAW B737-200 SRM 51-30-5 FIGURE 3. (M)
- [SDR ASAA0510310](https://openairdocs.org/sdr/ASAA0510310.md): Stringer · corroded · Sep 20, 2005 · N740AS · Boeing 737290C · Fuselage Main, Longeron/Stringer
  > YXX - FOUND CORROSION ON STRINGER AT BS 363-375 STRINGER 27 RIGHT. STRINGER 27 RT REPLACED FROM 363 TO 407 IAW B737-200 SRM 53-10-3. (M)
- [SDR ASAA0510309](https://openairdocs.org/sdr/ASAA0510309.md): Floorbeam · corroded · Sep 20, 2005 · N740AS · Boeing 737290C · Fuselage Main, Floor Beam
  > YXX - FOUND IN FORWARD CARGO PIT LOWER CHORD OF FLOORBEAM CORRODED AT BS 420 LBL 24. LOWER CHORD OF CABIN FLOORBEAM AT BS 420 LBL 24 WAS REPAIRED IAW ERO 4457 AND EA 53110-02491. REF ASA LOG 3017604 FOR WORK DETAILS. (M)
- [SDR ASAA0510308](https://openairdocs.org/sdr/ASAA0510308.md): Failsafe · cut · Sep 20, 2005 · N740AS · Boeing 737290C · Fuselage Main, Frame
  > YXX - FOUND FAIL/SAFE AT BS 360 TO BE CUT FOR ACCESS AT STRINGER 26 RT. REPAIRED IAW B737-200 SRM 51-40-3 FIGURE 1. (M)
- [SDR ASAA0510307](https://openairdocs.org/sdr/ASAA0510307.md): Attach Angle · corroded · Sep 20, 2005 · N740AS · Boeing 737290C · Fuselage Internal Mounting Structure
  > YXX - FOUND CORROSION ON SKIN TO FRAME ATTACH ANGLE BETWEEN STRINGER 28-27 LEFT AT BS 360. SKIN TO FRAME ATTACH ANGLE AT BS 360 BETWEEN STRINGER 27 LEFT AND 28 LEFT REPAIRED PER B737-200 SRM 53-10-4 FIGURE 8. (M)
- [SDR ASAA0510306](https://openairdocs.org/sdr/ASAA0510306.md): Doubler · corroded · Sep 20, 2005 · N740AS · Boeing 737290C · Fuselage Main, Plate/Skin
  > YXX - FOUND CORROSION ON BONDED DOUBLER AT BS 360 BETWEEN STRINGER 26R AND 27R. REPAIRED PER B737-200 SRM 51-40-3. (M)
- [SDR ASAA0510305](https://openairdocs.org/sdr/ASAA0510305.md): Stringer · corroded · Sep 20, 2005 · N740AS · Boeing 737290C · Fuselage Main, Longeron/Stringer
  > YXX - FOUND CORROSION ON STRINGER 26R AT BS 500A. REPAIRED PER B737-200 SRM 53-10-3 FIGURE 1. (M)
- [SDR ASAA0510304](https://openairdocs.org/sdr/ASAA0510304.md): Stringer · cut · Sep 20, 2005 · N740AS · Boeing 737290C · Fuselage Main, Longeron/Stringer
  > YXX - FOUND STRINGER 26L AT BS 334 TO BS 358 CUT. REPAIRED PER B737-200 SRM 53-10-3 FIGURE 1. (M)
- [SDR ASAA0510303](https://openairdocs.org/sdr/ASAA0510303.md): Stringer · damaged · Sep 20, 2005 · N740AS · Boeing 737290C · Fuselage Main, Longeron/Stringer
  > YXX - FOUND STRINGER 27L AT BS 395 CUT FOR ACCESS. REPAIRED PER B737-200 SRM 53-10-3 FIGURE 1. (M)
- [SDR ASAA0510302](https://openairdocs.org/sdr/ASAA0510302.md): Doubler · dented · Sep 20, 2005 · N740AS · Boeing 737290C · Fuselage Main, Structure
  > YXX - FOUND DOUBLER DAMAGED AT BS 360 BETWEEN STRINGER 27R TO 28L PLUS 14 INCHES. REPLACED DOUBLER PER B737-200 SRM 57-40-3 FIGURE 1. (M)
- [SDR ASAA0510299](https://openairdocs.org/sdr/ASAA0510299.md): Stringer · dented · Sep 15, 2005 · N740AS · Boeing 737290C · Fuselage Main, Longeron/Stringer
  > YXX - IN FORWARD PIT STRINGER 25 LEFT DENTED AT BS 51. REPLACED WITH FABRICATED REPAIR PART IAW B737-200 SRM 53-10-03. (M)
- [SDR ASAA0510298](https://openairdocs.org/sdr/ASAA0510298.md): Stringer · damaged · Sep 15, 2005 · N740AS · Boeing 737290C · Fuselage Main, Longeron/Stringer
  > YXX - FOUND TOOLING DAMAGE AT BS 440, STRINGER 7 RT. REPAIRED IAW B737-200 SRM 53-10-3 FIG 4. (M)
- [SDR ASAA0510297](https://openairdocs.org/sdr/ASAA0510297.md): Stringer · corroded · Sep 13, 2005 · N740AS · Boeing 737290C · Fuselage Main, Longeron/Stringer
  > YXX - FOUND CORROSION ON STRINGER 27 RT AT BS 360. REPAIRED BY REPLACEMENT. (M)
- [SDR ASAA0510296](https://openairdocs.org/sdr/ASAA0510296.md): Floorbeam · corroded · Sep 13, 2005 · N740AS · Boeing 737290C · Fuselage Main, Floor Beam
  > YXX - FOUND BEYOND LIMITS CORROSION ON BS 807 FLOORBEAM UPPER CAP AT LBL 24-LBL 45. REPAIRED IAW ERO 4554 AND EA 5310-02425 BY REINFORCEMENT OF CAP WITH STRAP. (M)
- [SDR ASAA0510295](https://openairdocs.org/sdr/ASAA0510295.md): Skin · corroded · Sep 12, 2005 · N740AS · Boeing 737290C · Fuselage Main, Plate/Skin
  > YXX - FOUND FUSELAGE SKIN BULGING AT BS 535 LEFT KEELBEAM. REPAIRED BY REPLACEMENT OF LEFT KEEL BEAM SECTION. (M)
- [SDR ASAA0510294](https://openairdocs.org/sdr/ASAA0510294.md): Shear Tie · corroded · Sep 12, 2005 · N740AS · Boeing 737290C · Fuselage Internal Mounting Structure
  > YXX - FOUND SKIN TO FRAME ANGLE CORRODED AT BS 360 BETWEEN STRINGER 25 RT AND 26 RT. REMOVED AND REPLACED FRAME TO SKIN ATTACH ANGLE PER B737-200 SRM 53-10-04 FIGURE 8. (M)
- [SDR ASAA0510293](https://openairdocs.org/sdr/ASAA0510293.md): Frame · corroded · Sep 12, 2005 · N740AS · Boeing 737290C · Fuselage Main, Frame
  > YXX - FOUND CORROSION ON FRAME TO SKIN ATTACH ANGLE AT BS 360 BETWEEN STRINGER 26-27 RT. REMOVED AND REPLACED FRAME TO SKIN ATTACH ANGLE PER SRM 53-10-4. (M)
- [SDR ASAA0510292](https://openairdocs.org/sdr/ASAA0510292.md): Bear Strap · scratched · Sep 7, 2005 · N740AS · Boeing 737290C · Fuselage Main, Plate/Skin
  > YXX - FOUND SCRATCHES ON BEAR STRAP AT BS 500 FROM STRINGER 3 LEFT TO 17 LEFT. PLT SUBMITTED. BEAR STRAP AT BS 500 FROM STRINGER 3 LEFT TO 17 LEFT WAS REPAIRED IAW ERO 4283 AND EA 5330-01982. (M)
- [SDR ASAA0510291](https://openairdocs.org/sdr/ASAA0510291.md): Skin · damaged · Sep 7, 2005 · N740AS · Boeing 737290C · Fuselage Main, Plate/Skin
  > YXX - FOUND FUSELAGE SKIN DAMAGED AT BS 996 1 INCH BELOW STRINGER 21 LEFT. DAMAGED FUSELAGE SKIN REPAIRED AT BS 996 1 INCH BELOW STRINGER 21 LEFT IAW B737-200 SRM 53-30-3 FIG 48. (M)
- [SDR ASAA0510290](https://openairdocs.org/sdr/ASAA0510290.md): Stringer · dented · Sep 7, 2005 · N740AS · Boeing 737290C · Fuselage Main, Longeron/Stringer
  > YXX - IN FORWARD CARGO PIT STRINGER 25 LEFT DENTED AT BS 408. REPLACED STRINGER PER B737-200 SRM 53-10-3. (M)

Next page: https://openairdocs.org/aircraft/N740AS/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 = 'N740AS' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N740AS/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.