# Service difficulty reports: JASC 5330

A list on [JASC 5330](https://openairdocs.org/jasc/5330.md).

Reports filed under 5330 · Fuselage Main, Plate/Skin, newest first.

Page 1 of 1,585 · 79,230 reports

- [SDR DALA2026102205832](https://openairdocs.org/sdr/DALA2026102205832.md): Skin · damaged · Oct 21, 2026 · N965AT · Boeing 717200
  > FOUND SEVERAL EXISTING LIGHTNING STRIKE DAMAGES COMMON TO STRINGER L2R IN THE KA1717 STC AREA, COMPLIED WITH ER/A 637562-14. (1877071) (AIRCRAFT GROUNDED).
- [SDR DALA2026102105788](https://openairdocs.org/sdr/DALA2026102105788.md): Skin · dented · Oct 20, 2026 · N970AT · Boeing 717200
  > FOUND DENTS AT LOWER FUSELAGE SKIN BETWEEN STA Y=495 & Y=507/L-28L & L-29, COMPLIED WITH ER/A 625374-14. (1876653) (AIRCRAFT GROUNDED).
- [SDR DALA2026101905723](https://openairdocs.org/sdr/DALA2026101905723.md): Skin · damaged · Oct 18, 2026 · N980AT · Boeing 717200
  > FOUND A DISCREPANT FASTENER HOLE WAS IDENTIFIED AT THE INTERSECTION OF FRAME Y503 AND LONGERON L1, AT THE FOURTH FASTENER LOCATION AFT OF THE FORWARD EDGE OF STC DOUBLER, CORRECTIVE ACTION: COMPLIED WITH ER/A 637350-14AD. (1871858) (AIRCRAFT GROUNDED).
- [SDR AALA202610203473](https://openairdocs.org/sdr/AALA202610203473.md): Skin · dented · Oct 16, 2026 · N316SE · Boeing 7378
  > AIRCRAFT IN BASE MAINTENANCE: DENT ON FUSELAGE SKIN BETWEEN STA 927 AND STA 951. MAINTENANCE INSTALLED FUSELAGE DOUBLE IAW EA 379203.
- [SDR SWIA2026101677757](https://openairdocs.org/sdr/SWIA2026101677757.md): Skin · corroded · Oct 16, 2026 · N913EV · Cndair CL6002B19
  > CORROSION ON FUSELAGE SKIN AROUND APU EXHAUST BETWEEN BS 640 - 682, STRINGERS 12R - 14R. BLENDED CORROSION ON FUSELAGE SKIN AROUND APU EXHAUST, PERFORMED UT REMAINING THICKNESS MEASUREMENT IAW NDTM PART 4, 51-00-001 AND FOUND TO BE ACCEPTABLE IAW REO 601R-
- [SDR IXXA20261016001](https://openairdocs.org/sdr/IXXA20261016001.md): Skin · cracked · Oct 16, 2026 · N443AZ · Boeing 767323
  > PERFORM REPLACEMENT OF THE FOLLOWING DAMAGE SECTION 43 FUSELAGE STRUCTURE FROM STA. 654 TO STA 785.9
- [SDR IXXA20261015007](https://openairdocs.org/sdr/IXXA20261015007.md): Skin · mechanic error · Oct 15, 2026 · N443AZ · Boeing 767323
  > MISSDRILLED HOLES AT R/H SKIN TEAR STRAP LOCATIONS FROM STA 654+44 TO STA 654+88 BETWEEN S-13R & S-9R AND FROM STA 654+110 TO STA 742 BETWEEN S-13R & S-11R.
- [SDR JR2R20261015724](https://openairdocs.org/sdr/JR2R20261015724.md): Skin · corroded · Oct 15, 2026 · N88359 · Emb ERJ170200LL
  > FWD CARGO SCUFF PLATE EXTERNAL SKIN LOCATED AT FR24-FR27 HAS MULTIPLE SPOTS OF CORROSION. REPAIRED PER ETD.
- [SDR IXXA20261015001](https://openairdocs.org/sdr/IXXA20261015001.md): Tear Strap · mechanic error · Oct 15, 2026 · N443AZ · Boeing 767323
  > MISRILLED HOLES AT LT SKIN TEAR STRAP
- [SDR AALA202610160189](https://openairdocs.org/sdr/AALA202610160189.md): Skin Panel · corroded · Oct 14, 2026 · N464AA · Airbus A321253NX
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FUSELAGE SKIN PANEL AROUND THE VACUUM GENERATOR EXHAUST BETWEEN FR 67 AND FR 70 BETWEEN A31R AND S32R - REPAIRED PER EA 380080
- [SDR SIMA20261014002](https://openairdocs.org/sdr/SIMA20261014002.md): Skin · corroded · Oct 14, 2026 · N774JG · Emb ERJ170100SE
  > CORROSION ON FORWARD EDGE OF LAV DRAIN BOX AFT SIDE OF FRAME 88 BETWEEN STRINGERS 29R-28R. (LEVEL 2 CORROSION) REPAIRED DAMAGE ON FORWARD EDGE OF LAV DRAIN BOX AFT SIDE OF FRAME 88 BETWEEN STRINGERS 29R-28R IAW SRM 53-23-60 REPAIR 01.
- [SDR IXXA202610140002](https://openairdocs.org/sdr/IXXA202610140002.md): Buttstrap · damaged · Oct 14, 2026 · N443AZ · Boeing 767323
  > CIRCUNFERENTIAL BUTT SPLICE STA 654+22 BETWEEN S-13L AND S-14L AN OVERSIZE RIVET HOLE NOTED WITH A.281" DIAMETER APROX
- [SDR IXXA20261014001](https://openairdocs.org/sdr/IXXA20261014001.md): Skin · out of limits · Oct 14, 2026 · N443AZ · Boeing 767323
  > L/H WINDOW B/S 654+33 AFT EDGE GAP IS OUT OF LIMITS AT.193 MAX LIMIT BEING.160
- [SDR DALA2026102105807](https://openairdocs.org/sdr/DALA2026102105807.md): Skin · gouged · Oct 13, 2026 · N929DZ · Boeing 737932ER
  > FOUND GOUGE ON FUSELAGE 12 INCHES FWD OF AFT CARGO DOOR. REPAIRED IAW ERA 637497-14. (9506948) AIRCRAFT WAS GROUNDED
- [SDR DALA2026101605689](https://openairdocs.org/sdr/DALA2026101605689.md): Skin · damaged · Oct 13, 2026 · N923DZ · Boeing 737932ER
  > LEFT FUSELAGE SKIN HAS DAMAGE ABOVE HORIZONTAL STAB NEAR SLIDING SEAL. STA 1088 AND 1104. REF ERA 6374949-14. (9153550) AIRCRAFT WAS GROUNDED
- [SDR N6WA2026101506](https://openairdocs.org/sdr/N6WA2026101506.md): Skin · corroded · Oct 13, 2026 · N581GJ · Cndair CL6002C11
  > EVALUATE POSSIBLE CORROSION ON SKIN FUSELAGE AT PANEL 195DR. REMOVED CORROSION ON SKIN FUSELAGE IN SEVERAL POINTS IAW SRM 51-21-06.
- [SDR N6WA2026101505](https://openairdocs.org/sdr/N6WA2026101505.md): Skin · scratched · Oct 13, 2026 · N581GJ · Cndair CL6002C11
  > EVALUATE SCRATCHES ON SKIN FUSELAGE LEFT BETWEEN BS 939 - 1115 AT PANEL 195DL. REMOVED SCRATCHES ON SKIN AT PANEL 195DL IAW SRM 51-00-01. NO DAMAGE ALLOWED IN THIS AREA IAW SRM 53-51-01.
- [SDR N6WA2026101504](https://openairdocs.org/sdr/N6WA2026101504.md): Skin · damaged · Oct 13, 2026 · N581GJ · Cndair CL6002C11
  > FOUND 2EA DAMAGED AREAS ON LOWER FUSELAGE SKIN AT FS977. PERFORMED PERMANENT REPAIR AT AFT FUSELAGE SKIN FS 977, STR 27 IAR EO #C550-53MR-127 REV. O.
- [SDR AALA202610152437](https://openairdocs.org/sdr/AALA202610152437.md): Skin · cracked · Oct 12, 2026 · N807AW · Airbus A319132
  > AIRCRAFT IN BASE MAINTENANCE: FASTIGUE CRACK RADIATING FROM FASTENER HOLE BETWEEN FR13-FR14 AND BETWEEN Z+780-Z+950ON LH SIDE. MAINTENANCE PERFORMED SKIN CUT OUT AND INSTALLED FABRICATED DOUBLER IAW EA 379994
- [SDR CALA2026101520382](https://openairdocs.org/sdr/CALA2026101520382.md): Skin · cracked · Oct 11, 2026 · N14219 · Boeing 737824
  > FOUND A CRACK AT FUSELAGE EXTERNAL SKIN WASTE VENT BS 917 STR 21 - 22. PERFORMED PERMANENT REPAIR ON FUSELAGE EXTERNAL SKIN WASTE VENT IAW SRM 53-70-01-2R-3. THIS REPAIR IS A CATEGORY B REPAIR
- [SDR DALA2026101305626](https://openairdocs.org/sdr/DALA2026101305626.md): Skin · dented · Oct 10, 2026 · N961AT · Boeing 717200
  > FOUR DENTS IDENTIFIED COMMON TO AFT INSTALLATION DOUBLER BETWEEN L2R AND L3R FRAME Y541 TO Y560. REPAIRED PER ER/A 637249-14. (1858631) AIRCRAFT WAS GROUNDED.
- [SDR UIEA2026100900973](https://openairdocs.org/sdr/UIEA2026100900973.md): Skin · cracked · Oct 10, 2026 · N649GT · Boeing 767375
  > DURING EO 6753A070 (SB 767-53A0100 R3/AD 2012-09-04 TERMINATING ACTION) OPEN-HOLE HFEC AT STA 955 R/H, A CRACK INDICATION WAS FOUND AT THE FAIL-SAFE STRAP, AND CORROSION WAS FOUND ON THE T-FITTING AND SKIN PANEL (P/N 145T3321-4) NEAR STR 22AR. REMAINING THICK
- [SDR DALA2026101305625](https://openairdocs.org/sdr/DALA2026101305625.md): Skin · cracked · Oct 9, 2026 · N978AT · Boeing 717200
  > DENT AND CRACK FUSELAGE SKIN STA Y=370-389, L-29R & L-30. REPAIRED PER ER/A 610692-14. (1857452) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026101205599](https://openairdocs.org/sdr/DALA2026101205599.md): Skin · mechanic error · Oct 9, 2026 · N920AT · Boeing 717200
  > DRILL START INDENTATIONS AT CABIN CEILING BS 927, BTWN STRINGER 3R & 4R. REPAIRED PER ER/A 637414-14. (1856706) AIRCRAFT WAS GROUNDED.
- [SDR UIEA2026092100889](https://openairdocs.org/sdr/UIEA2026092100889.md): Doubler · no discrepancy · Oct 9, 2026 · N419MC · Boeing 74748EF
  > SECT 41 LAP JOINT INSP: EXISTING DOUBLERS (06 EA) ON S-14L STA 140-160, S-44L STA 240-260, S-44R STA 240-260, S39R STA 380-420, S45L STA 400-420 AND S45R STA 400-420 FOUND THE REPAIR NOT CONFIRMED TO SRM 53-00-01, REPAIR 10, 12 OR 16(<P >DOUBLERS AT STA 240 -
- [SDR UIEA2026100500952](https://openairdocs.org/sdr/UIEA2026100500952.md): Doubler · misinstalled · Oct 9, 2026 · N419MC · Boeing 74748EF
  > SEC 42 LAP JOINT INSP OF EXISTING DOUBLERS (02 EA) ON S39L, STA 940-960 AND S39R, STA 920-960; FOUND THE REPAIR NOT CONFIRMED TO SRM 53-00-01, REPAIR 10,12 OR 16. BODY FAIRING PANEL REMOVED & REINSTALLED IAW AMM 53-51-01-004-001, REV 117 & AMM 53-51-01-404-00
- [SDR UIEA2026100600964](https://openairdocs.org/sdr/UIEA2026100600964.md): Doubler · misinstalled · Oct 9, 2026 · N419MC · Boeing 74748EF
  > SECT 46 LAP JOINT INSP OF EXISITNG DOUBLERS (05 EA), STRINGER 14L, BS 1980-2020, S12L, BS 1720-1740, S12L, STA 2140-2160, S34L, STA 1640-1960 AND S40L, STA 1640-1820; FOUND THE REPAIR NOT CONFORMED TO SRM 53-00-01, REPAIR 10, 12 OR 16. REPAIRED IAW EN 3737-
- [SDR SWIA2026100877552](https://openairdocs.org/sdr/SWIA2026100877552.md): Skin · dented · Oct 8, 2026 · N304SY · Emb ERJ170200LL
  > DENTED FWD FUSELAGE LT SKIN JUST BEHIND THE LI DOOR BTWN FRAMES 21-22, STRINGERS 15L-16L. THE TOTAL AREA OF THE IS 4 INCHES BY 325 INCHES WITH A DEPTH OF 0186 INCH. REPAIRED THE SKIN IAW ETD2026-170-017154, REV-.
- [SDR DALA2026101205589](https://openairdocs.org/sdr/DALA2026101205589.md): Skin · cracked · Oct 8, 2026 · N808DN · Boeing 737932ER
  > DURING HFEC INSP. ON CUT OUT OF UPPER SKIN. STRINGER 2ND HOLE FROM CUT OUT IS CRACKED. ALSO CUT OUT ON STRINGER 24 CUT OFF WHEEL DAMAGE AFT ON CUT OUT. REPLACED STRINGER 24L PER ERA 637291-14 REV A. STEP 14, AND SRM 51-40-02. (1855525) AIRCRAFT WAS GROUNDED
- [SDR DALA2026101205588](https://openairdocs.org/sdr/DALA2026101205588.md): Skin · punctured · Oct 8, 2026 · N808DN · Boeing 737932ER
  > DTE, ER/A 637291-14 REV A FOR SKIN REPAIR OF PUNCTURE AT STA 203.8 AND STR24L. REF ERA 637291-14. (1855311) AIRCRAFT WAS GROUNDED.
- [SDR AALA202610094763](https://openairdocs.org/sdr/AALA202610094763.md): Skin · corroded · Oct 8, 2026 · N810NN · Boeing 737823
  > AIRCRAFT IN BASE MAINTENANCE: AFT CARGO SKIN CORROSION AT BS 767-807, STR 27R. ACCOMPLISHED REPAIR DOUBLER INSTALL AND REPAIR INSTRUCTIONS IAW EA 379610.
- [SDR DALA2026101305608](https://openairdocs.org/sdr/DALA2026101305608.md): Skin · damaged · Oct 7, 2026 · N6707A · Boeing 757232
  > LIGHTNING STRIKE ON FUSELAGE SKIN BS 328, 348, 360, AND 391. REPAIRED IAW SRM 53-00-01-2R, PROCEDURE 6. (1853249)(AIRCRAFT GROUNDED)
- [SDR DALA2026101305607](https://openairdocs.org/sdr/DALA2026101305607.md): Skin · damaged · Oct 7, 2026 · N6707A · Boeing 757232
  > LIGHTNING STRIKE ON FUSELAGE SKIN BS 328 - 348, 360, & 391, REPAIRED IAW SRM 53-00-01-2R, PROCEDURE 6. (1853238)(AIRCRAFT GROUNDED)
- [SDR UIEA2026093000932](https://openairdocs.org/sdr/UIEA2026093000932.md): Skin · gouged · Oct 7, 2026 · N486MC · Boeing 74745EF
  > DURING INSPECTION OF THE LOWER LOBE FWD CARGO DOOR STRINGER 34R SKIN LAP SPLICE, A GOUGE WAS FOUND C/T UPPER SKIN. WORK ACCOMPLISHED IAW EN#3792-26, REV 0. NO FURTHER DEFECTS NOTED.
- [SDR IPXA2026101512243](https://openairdocs.org/sdr/IPXA2026101512243.md): Skin · dented · Oct 6, 2026 · N127UP · Airbus A300F4622R
  > LOWER FUSELAGE, BTWN FR 51 TO 52, LH SIDE, NEXT TO MLG DOOR CUTOUT, EXTERNAL SURFACE, SKIN HAS A DENT W/ GOUGE. ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH EO-98862-REQ1 AND STE PNA EA 300-5315-27-A4660, REV-.
- [SDR AALA202610108075](https://openairdocs.org/sdr/AALA202610108075.md): Skin Panel · cracked · Oct 6, 2026 · N174US · Airbus A321211
  > AIRCRAFT IN BASE MAINTENANCE: CRACKED FUSELAGE SKIN PANEL FASTENER HOLE AT FR 14 AND S11R - REPAIRED FUSELAGE SKIN PANEL PER EA 379758
- [SDR AALA202610071210](https://openairdocs.org/sdr/AALA202610071210.md): Skin Panel · cracked · Oct 6, 2026 · N174US · Airbus A321211
  > AIRCRAFT IN BASE MAINTENANCE: CRACKED FUSELAGE SKIN PANEL AT FR 14 AND S11L - REPAIRED SKIN PANEL PER EA 379757
- [SDR CALA2026100720187](https://openairdocs.org/sdr/CALA2026100720187.md): Skin · cracked · Oct 6, 2026 · N78008 · Boeing 777224
  > ONE HOLE FOUND CRACKED ON RT FUSELAGE SKIN LAYER UNDER LONGERON FITTING. REPAIRED IAW EA 5310-07557, OP 007.
- [SDR QMLA2026100620076](https://openairdocs.org/sdr/QMLA2026100620076.md): Doubler · cracked · Oct 6, 2026 · N138LN · Urocop EC135P2
  > DURING INSPECTIONS FOUND REAR DOUBLER CRACK. ALSO NEXT TO THAT THE INSIDE REINFORCEMENT CRACKED
- [SDR JR2R20261006187](https://openairdocs.org/sdr/JR2R20261006187.md): Skin · corroded · Oct 6, 2026 · N85320 · Emb ERJ170200LL
  > UPON REMOVAL OF FWD LOWER DRAIN MAST, EXTERNAL SKIN FOUND CORRODED. REPAIRED PER ETD.
- [SDR AALA202610089601](https://openairdocs.org/sdr/AALA202610089601.md): Skin · corroded · Oct 5, 2026 · N819NN · Boeing 737823
  > AIRCRAFT IN BASE MAINTENANCE: LH RAM AIR FWD DOOR INTERNAL SKIN CORRODED. REMOVED AND REPLACED LH RAM AIR FWD DOOR MODULATION PANEL IAW AMM 21-51-23.
- [SDR 9WGA2026100754501](https://openairdocs.org/sdr/9WGA2026100754501.md): Skin · ground damage · Oct 5, 2026 · N9WGA · Doug MD11F
  > AT STATION NSY, DURING CARGO LOADING, ONE PALLET FELL OFF THE K-LOADER AND HIT THE FUSELAGE ABOVE WATER SERVICING PANEL BS 755, MX CONTROL INFORMED OF SITUATION, STS ENGINEERING CONTACTED FOR WGA ASSISTANCE, SEE LOG PAGE 238614, ITEM M1, EVALUATION OF FUSELAGE
- [SDR IPXA2026101280317](https://openairdocs.org/sdr/IPXA2026101280317.md): Skin · corroded · Oct 3, 2026 · N402UP · Boeing 75724APF
  > AFTER REMOVAL OF ADF ANTENNA FOUND UPPER FUSELAGE SKIN WITH DEEP PITTING CORROSION AND TOOLING MARKS.
- [SDR ABXA20261003452](https://openairdocs.org/sdr/ABXA20261003452.md): Skin · damaged · Oct 3, 2026 · N760CK · Boeing 767341
  > DURING C 6 CHECK IN AT KALITTA MTX FOUND CROWN SKIN DAMAGED AT BS 1467 LBL 12. TT04. MTX ACCOMPLISHED REPAIR OF CROWN SKIN AT BS 1467 LBL 12 IAW SRM 53-00-01, REPAIR 14.
- [SDR SWAA2026101908490](https://openairdocs.org/sdr/SWAA2026101908490.md): Skin · cracked · Oct 2, 2026 · N8626B · Boeing 7378H4
  > EXISTING FASTENER HOLE HAD A CRACK INDICATION AT BS 727G+6.5, IAW EA 26-153-02701 THE CONFIGURATION IS ACCEPTABLE.
- [SDR SWAA2026101500242](https://openairdocs.org/sdr/SWAA2026101500242.md): Doubler · cracked · Oct 2, 2026 · N8697C · Boeing 7378H4
  > EGPR SURROUND DOUBLER CRACKED AT LOWER FLANGE. ACCOMPLISHED REPAIR ON EGPR SURROUND DOUBLER LOWER FLANGE IAW SRM 53-10-15-2R-4.
- [SDR DALA2026100505510](https://openairdocs.org/sdr/DALA2026100505510.md): Skin · damaged · Oct 2, 2026 · N998AT · Boeing 717200
  > FUSELAGE SKIN FS 294-351 S-28R TO S-27L DAMAGED. REPAIRED PER ER/A 590835-14. (1845326) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026100505499](https://openairdocs.org/sdr/DALA2026100505499.md): Waste Box · corroded · Oct 2, 2026 · N322DU · Airbus BD5001A11
  > LAVATORY WASTE BOX FWD RIGHT HAND CORNER (DOOR SEAL AREA) HAS CORROSION. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 081-0001:0591-0301/004 00127 COMPLIED WITH ER/A 637082-14 PRI REV 0, 1, 2, AND ER/A 637082-14 REV ORI
- [SDR CALA2026100520095](https://openairdocs.org/sdr/CALA2026100520095.md): Skin · cracked · Oct 2, 2026 · N78008 · Boeing 777224
  > ONE HOLE FOUND CRACKED AT LONGERON AREA. THE FUSELAGE SKIN AT BS 993-1035, S35R-37R WAS REPAIRED IAW EA 5310-07557, REV C.
- [SDR CALA2026100520092](https://openairdocs.org/sdr/CALA2026100520092.md): Skin · cracked · Oct 2, 2026 · N78008 · Boeing 777224
  > TWO HOLES FOUND CRACKED ON RT UNDERWING LONGERON AREA. FUSELAGE SKIN AT BS 993-1035, S35-37R REPAIRED IAW EA 5310-07557, REV C.

Next page: https://openairdocs.org/jasc/5330/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 jasc_code = '5330'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/jasc/5330/reports

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